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MEMPHIS - 2025

2025‌Activity reportProject-TeamMEMPHIS‌​‌

RNSR: 201521153G
  • Research center​​ Inria Centre at the​​​‌ University of Bordeaux
  • In‌ partnership with:Université de‌​‌ Bordeaux
  • Team name: Modeling​​ Enablers for Multi-PHysics and​​​‌ InteractionS
  • In collaboration with:‌Institut de Mathématiques de‌​‌ Bordeaux (IMB)

Creation of​​ the Project-Team: 2016 October​​​‌ 01

Each year, Inria‌ research teams publish an‌​‌ Activity Report presenting their​​ work and results over​​​‌ the reporting period. These‌ reports follow a common‌​‌ structure, with some optional​​ sections depending on the​​​‌ specific team. They typically‌ begin by outlining the‌​‌ overall objectives and research​​ programme, including the main​​​‌ research themes, goals, and‌ methodological approaches. They also‌​‌ describe the application domains​​​‌ targeted by the team,​ highlighting the scientific or​‌ societal contexts in which​​ their work is situated.​​​‌

The reports then present​ the highlights of the​‌ year, covering major scientific​​ achievements, software developments, or​​​‌ teaching contributions. When relevant,​ they include sections on​‌ software, platforms, and open​​ data, detailing the tools​​​‌ developed and how they​ are shared. A substantial​‌ part is dedicated to​​ new results, where scientific​​​‌ contributions are described in​ detail, often with subsections​‌ specifying participants and associated​​ keywords.

Finally, the Activity​​​‌ Report addresses funding, contracts,​ partnerships, and collaborations at​‌ various levels, from industrial​​ agreements to international cooperations.​​​‌ It also covers dissemination​ and teaching activities, such​‌ as participation in scientific​​ events, outreach, and supervision.​​​‌ The document concludes with​ a presentation of scientific​‌ production, including major publications​​ and those produced during​​​‌ the year.

Keywords

Computer​ Science and Digital Science​‌

  • A6. Modeling, simulation and​​ control
  • A6.1.1. Continuous Modeling​​​‌ (PDE, ODE)
  • A6.1.5. Multiphysics​ modeling
  • A6.2.1. Numerical analysis​‌ of PDE and ODE​​
  • A6.3.1. Inverse problems
  • A6.3.2.​​​‌ Data assimilation
  • A6.3.4. Model​ reduction
  • A6.5.1. Solid mechanics​‌
  • A6.5.2. Fluid mechanics
  • A9.2.​​ Machine learning

Other Research​​​‌ Topics and Application Domains​

  • B2.2.1. Cardiovascular and respiratory​‌ diseases
  • B4.2. Nuclear Energy​​ Production
  • B4.3.2. Hydro-energy
  • B4.3.3.​​​‌ Wind energy
  • B5.2.3. Aviation​
  • B5.2.4. Aerospace
  • B5.5. Materials​‌

1 Team members, visitors,​​ external collaborators

Research Scientists​​​‌

  • Michel Bergmann [INRIA​, Senior Researcher,​‌ until Oct 2025,​​ HDR]
  • Michele Giuliano​​​‌ Carlino [ONERA,​ until Oct 2025]​‌
  • Alessia Del Grosso [​​INRIA, ISFP,​​​‌ until Oct 2025]​
  • Tommaso Taddei [INRIA​‌, Researcher, until​​ Aug 2025]

Faculty​​​‌ Members

  • Angelo Iollo [​Team leader, UNIV​‌ BORDEAUX, Professor Delegation​​, until Oct 2025​​​‌, HDR]
  • Angelo​ Iollo [Team leader​‌, UNIV BORDEAUX,​​ Professor, from Nov​​​‌ 2025, HDR]​
  • Afaf Bouharguane [UNIV​‌ BORDEAUX, Associate Professor​​, HDR]

Post-Doctoral​​​‌ Fellows

  • Joyce Ghantous [​INRIA, Post-Doctoral Fellow​‌, until Aug 2025​​]
  • Ivan Kharsansky Atallah​​​‌ [ONERA, Post-Doctoral​ Fellow, from Feb​‌ 2025 until Oct 2025​​]

PhD Students

  • Maxime​​​‌ Chapron [ONERA,​ until Sep 2025]​‌
  • Elise Declerck [ONERA​​, until Oct 2025​​​‌]
  • Jon Labatut [​ONERA, until Sep​‌ 2025]
  • Karl Maroun​​ [Université de Poitiers​​​‌, until Jan 2025​]
  • Abdessamad Moussaddak [​‌EDF, CIFRE,​​ until Oct 2025]​​​‌
  • Marc-Olivier Potin [ONERA​, until Oct 2025​‌]
  • Alexis Tardieu [​​UNIV BORDEAUX, ATER​​​‌, until Mar 2025​]
  • Mathias Truel [​‌INGELIANCE, CIFRE,​​ until Oct 2025]​​​‌
  • Alexis Valls [INRIA​]

Interns and Apprentices​‌

  • Sofia Curto [INRIA​​, Intern, from​​​‌ Mar 2025 until Sep​ 2025]
  • Giorgia Lanciotti​‌ [ONERA, Intern​​, from Mar 2025​​​‌ until Aug 2025]​
  • Samuel Oyhanto [INRIA​‌, Intern, from​​ Aug 2025 until Sep​​​‌ 2025]
  • Samuel Oyhanto​ [INRIA, Intern​‌, from Jun 2025​​ until Jul 2025]​​
  • Giovanni Polizzi [INRIA​​​‌, Intern, from‌ Feb 2025 until Jul‌​‌ 2025]

Administrative Assistant​​

  • Anne-Laure Gautier [INRIA​​​‌]

External Collaborators

  • Philippe‌ Depouilly [CNRS]‌​‌
  • Tommaso Taddei [UNIV​​ SAPIENZA , from Sep​​​‌ 2025 until Oct 2025‌]

2 Overall objectives‌​‌

2.1 Multi-physics numerical modeling​​

2.1.1 Reduced-order models: convergence​​​‌ between PDE models and‌ data

Unprecedented opportunities exist‌​‌ to directly use already​​ collected computational or experimental​​​‌ data to improve and‌ build predictive models that‌​‌ can be used online​​ for the simulation of​​​‌ parametric problems, robust design,‌ and control in science‌​‌ and engineering. In this​​ regard, our goal is​​​‌ to combine mechanistic causal‌ models based on partial‌​‌ differential equations (PDEs) with​​ large data sets to​​​‌ reduce the marginal cost‌ of predictions.

Reduced-order models‌​‌ (ROMs) are our main​​ tool for this purpose.​​​‌ ROMs are parametric mathematical‌ models derived from the‌​‌ full set of PDEs​​ using previously computed solutions.​​​‌ In many applications, the‌ solution space turns out‌​‌ to be low-dimensional, so​​ one can trade a​​​‌ minimal loss of accuracy‌ for speed and scalability.‌​‌ ROMs counteract the curse​​ of dimensionality by significantly​​​‌ reducing computational complexity.

Overall,‌ ROMs have reached a‌​‌ certain level of maturity​​ during the last decade,​​​‌ allowing their implementation in‌ large-scale industrial codes, mainly‌​‌ in structural mechanics. Nevertheless,​​ some hard points stand.​​​‌ Parametric problems governed by‌ strong advection fields or‌​‌ sensibly compact-support solutions such​​ as moving shocks suffer​​​‌ from a limited possibility‌ of dimensional reduction and,‌​‌ at the same time,​​ insufficient generalization of the​​​‌ model (out-of-sample solutions). The‌ main reason for this‌​‌ is that the solution​​ space is usually approximated​​​‌ by an affine or‌ linear representation, which is‌​‌ intrinsically broad band for​​ such problems.

We have​​​‌ worked on the development‌ of model order reduction‌​‌ (MOR) techniques for nonlinear,​​ advection-dominated problems, with emphasis​​​‌ on projection-based Galerkin and‌ Petrov-Galerkin ROMs. First, we‌​‌ worked on the development​​ of effective sampling strategies​​​‌ to reduce training costs.‌ Second, we developed nonlinear,‌​‌ registration-based approximation techniques, to​​ overcome limitations of linear​​​‌ approximation methods (e.g., proper‌ orthogonal decomposition, POD) to‌​‌ deal with strong advection​​ fields. Third, we developed​​​‌ hybrid formulations that combine‌ reduced-order and full-order models‌​‌ to deal with complex​​ flow features and/or complex​​​‌ parameterizations.

2.1.2 Schemes for‌ Hierarchical and Chimera meshes,‌​‌ multi-physics and asymptotic limits​​

The schemes we have​​​‌ developed aim at simulating‌ complex multiphysics phenomena through‌​‌ appropriate PDE modeling, automatic​​ implicit geometry representation (level​​​‌ sets), hierarchical Cartesian schemes‌ (quad-octrees), parallel simulations, and‌​‌ accurate treatment of boundaries.​​ Discretization schemes on hierarchical​​​‌ meshes allow multiscale solution‌ of PDEs on non-body-fitted‌​‌ meshes with a drastic​​ reduction in computational setup​​​‌ overhead. The key idea‌ is to use an‌​‌ octree mesh to approximate​​ the solution fields, while​​​‌ the geometry is captured‌ by level set functions.‌​‌ The boundary conditions are​​ determined by appropriate interpolation​​​‌ methods to achieve sufficient‌ accuracy. This approach eliminates‌​‌ the need for boundary​​ conforming meshes, which require​​​‌ time-consuming and error-prone mesh‌ generation procedures, and opens‌​‌ the door to easy​​​‌ parallel simulation of very​ complex geometries.

One of​‌ the limitations of this​​ approach is that a​​​‌ mesh with a fixed​ aspect ratio is not​‌ optimal for very anisotropic​​ fields such as boundary​​​‌ layers. For such cases,​ we explored the idea​‌ of using a body-fitted​​ grid near the immersed​​​‌ obstacles and a hierarchical​ mesh in the background.​‌ Essentially, we use the​​ techniques we have developed​​​‌ to impose boundary conditions​ on non-body-matched meshes further​‌ from the boundary, where​​ the solution is smoother​​​‌ and more isotropic. Our​ current investigations build on​‌ discontinuous Galerkin (DG) methods​​ / ADER approaches to​​​‌ combine efficient interpolation strategies​ at the grid interfaces​‌ and compact reconstruction of​​ the data at the​​​‌ grid level.

A differnt​ approach we have investigated​‌ was a space–time FEM/FVM​​ scheme on moving Chimera​​​‌ (overset) grids for linear​ and nonlinear advection–diffusion problems,​‌ with compact and accurate​​ coupling across overlapping regions​​​‌ via space–time interpolation polynomials​ and a FEM-predictor/FVM-corrector formulation​‌ with a new space–time​​ stabilization. The method is​​​‌ extended to incompressible Navier–Stokes​ equations on evolving domains​‌ using a fractional-step approach​​ and a hybrid gradient​​​‌ discretization that automatically handles​ grid overlap, achieving uniform​‌ second-order accuracy in space​​ and time without spurious​​​‌ artifacts.

Part of our​ activity has been dedicated​‌ to improve schemes for​​ all Mach number flows​​​‌ in both fluid dynamics​ and continuum mechanics. Phenomena​‌ of interest involve fluid​​ flows and elastic materials​​​‌ whose deformations are investigated​ within a monolithic Eulerian​‌ framework. With this approach​​ any material (gas, liquid​​​‌ or solid) can be​ described with the same​‌ system of conservation equations​​ and a suitable general​​​‌ formulation of the constitutive​ law.

These schemes are​‌ accurate in computing steady​​ state solutions as well​​​‌ as in approximating material​ wave propagation in various​‌ Mach regimes and different​​ materials. We studied methods​​​‌ to overcome the need​ to solve for auxiliary​‌ relaxation variables while preserving​​ the properties of the​​​‌ linearly implicit schemes. To​ achieve this, we split​‌ the stiff relaxation source​​ terms from the fluxes​​​‌ and then reformulate the​ homogeneous part in an​‌ elliptic form. Further research​​ on obtaining all Mach​​​‌ methods by including multi-dimensional​ knowledge in the numerical​‌ scheme is also being​​ conducted. More specifically, we​​​‌ envisage to exploit a​ nodal pressure that depends​‌ on all the cells​​ around the given node​​​‌ and naturally encompasses a​ consistent discretization of the​‌ divergence of the velocity​​ vector.

3 Research program​​​‌

Coherently with our investigation​ approach, we start from​‌ real-world applications to identify​​ key methodological problems, then,​​​‌ we study those problems​ and develop new methods​‌ to address them; finally,​​ we implement these methods​​​‌ for representative test cases​ to demonstrate their practical​‌ relevance.

MEMPHIS has already​​ evolved in a new​​​‌ project-team, MONHADE, in collaboration​ with Onera. The objective​‌ of the MONHADE team​​ is to develop hybrid​​​‌ numerical and physical modelling​ methodologies that combine partial​‌ differential equation–based models with​​ high-fidelity data, ensuring explainability,​​​‌ accuracy, and robustness, while​ remaining computationally efficient. These​‌ methods target performance prediction,​​ parametric optimisation, control, and​​ data assimilation for fluid​​​‌ systems interacting with structures.‌

3.1 Numerical models

We‌​‌ aim to further develop​​ automated model-order reduction (MOR)​​​‌ procedures for large-scale systems‌ in computational mechanics —‌​‌ here, automated refers to​​ the ability to complete​​​‌ the analysis with minimal‌ user intervention. First, we‌​‌ wish to combine nonlinear​​ MOR with mesh adaptation​​​‌ to simultaneously learn rapid‌ and reliable ROMs and‌​‌ effective high-fidelity discretizations over​​ a range of parameters.​​​‌ Second, we wish to‌ develop component-based MOR procedures‌​‌ to build inter-operable components​​ for steady and unsteady​​​‌ nonlinear PDEs: towards this‌ end, we should develop‌​‌ efficient localized training procedures​​ to build local ROMs​​​‌ for each archetype component,‌ and also domain decomposition‌​‌ techniques to glue together​​ the local models for​​​‌ prediction. We also wish‌ to develop and analyze‌​‌ hybrid approaches that combine​​ and merge first-principle models​​​‌ with data-fit models, and‌ also full-order and reduced-order‌​‌ models for prediction of​​ global engineering quantities of​​​‌ interest.

We envision that‌ several methods that are‌​‌ currently developed in the​​ team can be complemented​​​‌ by available tools from‌ machine learning: representative examples‌​‌ include — but are​​ not limited to —​​​‌ solution clustering, optimal sampling,‌ classification. In this respect,‌​‌ a leap forward in​​ industrial applications that we​​​‌ will pursue is without‌ doubts the possibility of‌​‌ capitalizing on previous experience​​ drawn from already acquired​​​‌ simulations to build non-intrusive‌ models that combine non-linear‌​‌ interpolations and non-linear regression.​​ New perspectives in this​​​‌ direction are offered by‌ the Chair Onera-Nouvelle Aquitaine‌​‌ (cf. Regional initiatives).

As​​ regards the work on​​​‌ numerical discretization of PDEs,‌ compared to the previous‌​‌ evaluation, we focus on​​ the representation of the​​​‌ solution in each computational‌ cell by adopting a‌​‌ DG/ADER approach to improve​​ the resolution of solution's​​​‌ discontinuities. This approach is‌ complemented with a Chimera‌​‌ grid at the boundaries​​ in order to improve​​​‌ accuracy by a body‌ fitted mesh avoiding grid‌​‌ generation complexity for a​​ general, possibly varying, geometrical​​​‌ topology. The thesis of‌ Alexis Tardieu, which started‌​‌ in October 2021 and​​ is funded by the​​​‌ University of Bordeaux, studies‌ this approach.

In parallel,‌​‌ we continue our exploration​​ of schemes in asymptotic​​​‌ regimes such as low-‌ and high Mach numbers‌​‌ for multi-material flows. We​​ aim for schemes that​​​‌ circumvent the problem of‌ accuracy and time stepping‌​‌ in such regimes: the​​ ultimate goal is to​​​‌ devise asymptotic-preserving schemes that‌ are able to capture‌​‌ phenomena at the time​​ scale of the fast​​​‌ waves and of the‌ material waves with the‌​‌ same accuracy. For such​​ a purpose, a new​​​‌ path based on numerical‌ schemes with multi-dimensional knowledge‌​‌ is also being explored.​​

3.2 Applications

For energy​​​‌ applications, we will continue‌ our investigations on wave‌​‌ energy converters and windturbines.​​ Relative to wave energy​​​‌ converters, we are developing‌ multifidelty models that couple‌​‌ the incompressible Navier-Stoke equations​​ (NSE) around the floater​​​‌ with a Proper Orthogonal‌ (POD) ROM or a‌​‌ simplified-physics model elsewhere.

We​​ are also collaborating with​​​‌ EDF to devise effective‌ ROMs for parametric studies.‌​‌ In this collaboration, we​​​‌ emphasize the implementation of​ projection-based ROMs for real-world​‌ applications exploiting industrial codes.​​

  • In December 2023, Abdessamad​​​‌ Moussaddak started his PhD​ thesis on model reduction​‌ for river and coastal​​ hydraulics.

In the framework​​​‌ of RedLUM ANR project​ we develop and apply​‌ mathematical and computational tools​​ for real-time estimation and​​​‌ short-term prediction of three-dimensional​ fluid flows using limited​‌ computational resources, by coupling​​ data, numerical simulations, and​​​‌ sparse flow measurements. To​ achieve these goals, the​‌ problem dimensionality are significantly​​ reduced through data-driven and​​​‌ reduced-order models, while the​ errors induced by dimensionality​‌ reduction will be quantified​​ using a stochastic, physics-informed,​​​‌ multiscale parametrization.

The software​ development will be continued.​‌ We will pursue the​​ development of the NEOS​​​‌ library: NEOS will be​ distributed in open source​‌ LGPL-3.0. The HIWIND software​​ will be rewritten based​​​‌ on NEOS library.

4​ Application domains

4.1 Energy​‌ conversion

We apply the​​ methods developed in our​​​‌ team to the domain​ of wind engineering and​‌ sea-wave converters. In Figure​​ 1, we show​​​‌ results of a numerical​ model for a sea-wave​‌ energy converter. We here​​ rely on a monolithic​​​‌ model to describe the​ interaction between the rigid​‌ floater, air and water;​​ material properties such as​​​‌ densities, viscosities and rigidity​ vary across the domain.​‌ The appropriate boundary conditions​​ are imposed at interfaces​​​‌ that arbitrarily cross the​ grid using adapted schemes​‌ built thanks to geometrical​​ information computed via level​​​‌ set functions 62.​ The background method for​‌ fluid-structure interface is the​​ volume penalization method 48​​​‌ where the level set​ functions is used to​‌ improve the degree of​​ accuracy of the method​​​‌ 5 and also to​ follow the object. The​‌ underlined mathematical model is​​ unsteady, and three dimensional;​​​‌ numerical simulations based on​ a grid with 𝒪​‌(108)​​ degrees of freedom are​​​‌ executed in parallel using​ 512 CPUs.

Figure 1

See-wave converter​‌

Figure 1: numerical​​ modeling of a sea-wave​​​‌ converter by a monolithic​ model and Cartesian meshes.​‌
Figure 2.a
  
Figure 2.b

Wind turbine

Figure 2​​: Aerogust project. Left:​​​‌ met mast after its​ installation. Right: flow around​‌ a NREL wind turbine​​ rotor (as predicted by​​​‌ NaSCar).

In the context​ of the Aerogust (Aeroelastic​‌ gust modelling) European project,​​ together with Valorem, we​​​‌ investigated the behavior of​ wind turbine blades under​‌ gust loading. The aim​​ of the project was​​​‌ to optimize the design​ of wind turbine blades​‌ to maximize the power​​ extracted. A meteorological mast​​​‌ (Figure 2(a)) has​ been installed in March​‌ 2017 in Brittany to​​ measure wind on-site: data​​​‌ provided by the mast​ have been exploited to​‌ initialize the mathematical model.​​ Due to the large​​​‌ cost of the full-order​ mathematical model, we relied​‌ on a simplified model​​ 58 to optimize the​​​‌ global twist. Then, we​ validated the optimal configuration​‌ using the full-order Cartesian​​ model based on the​​​‌ NaSCar solver. Figure 2​(b) shows the flow​‌ around the optimized optimized​​ wind turbine rotor.

4.2​​​‌ Schemes for turbulent flow​ simulations using Octrees

We​‌ have initially developed and​​ tested a 3D first-order​​ Octree code for unsteady​​​‌ incompressible Navier-Stokes equations for‌ full windmill simulations with‌​‌ an LES model and​​ wall laws. We have​​​‌ validated this code on‌ Occigen for complex flows‌​‌ at increasing Reynolds numbers.​​ This step implied identifying​​​‌ stable and feasible schemes‌ compatible with the parallel‌​‌ linear Octree structure. The​​ validation has been conducted​​​‌ with respect to the‌ results of a fully‌​‌ Cartesian code (NaSCAR) that​​ we run on Turing​​​‌ (with significantly more degrees‌ of freedom) and with‌​‌ respect to experimental results.​​

Subsequently, we have developed​​​‌ a second-order Octree scheme‌ that has been validated‌​‌ on Occigen for a​​ sphere at a moderate​​​‌ Reynolds number ( Re‌ =500), see‌​‌ Table 1. Then,​​ for a cylinder at​​​‌ ( Re =140000‌) (Figures 3(a)‌​‌ and 3(b)), close​​ to real applications, we​​​‌ have preliminary validation results‌ for the second-order scheme‌​‌ with respect to experimental​​ drag coefficient (Table 2​​​‌). Additional resources will‌ be asked on Occigen‌​‌ to complete the study.​​

Table 1: Flow past​​​‌ a sphere at Re‌ =500. Results‌​‌ in the literature are​​ spread between CD​​​‌=0.48‌ and CD=‌​‌0.52.​​
Mesh Δ x min​​​‌ number of cells C‌D (1st-order‌​‌ scheme) CD (2​​nd-order scheme)
1​​​‌ 0 . 094 0‌ . 72 · 10‌​‌ 5 N.A. 0 .​​ 526
2 0 .​​​‌ 047 4 . 9‌ · 10 5 0‌​‌ . 595 0 .​​ 522
3 0 .​​​‌ 023 4 . 7‌ · 10 6 0‌​‌ . 546 0 .​​ 492
4 0 .​​​‌ 012 37 . 6‌ · 10 6 0‌​‌ . 555 0 .​​ 496
Table 2: Flow​​​‌ past a sphere at‌ Re =14000.‌​‌
Case C D
Octree,​​ 1st-order scheme​​​‌ 1 . 007
Octree,‌ 2nd-order scheme‌​‌ 1 . 157
Cartesian​​ 1 . 188
Experimental​​​‌ estimate 54 1 .‌ 237
Figure 3.a
  
Figure 3.b

Turbulent simulations

Figure‌​‌ 3: flow past​​ a cylinder at Re​​​‌ =140000. Left:‌ vorticity contour lines. Right:‌​‌ streamwise velocity section and​​ grid for the second-order​​​‌ Octree scheme.

4.3 Vascular‌ flows

A new research‌​‌ direction pursued by the​​ team is the mathematical​​​‌ modelling of vascular blood‌ flows in arteries. Together‌​‌ with the start-up Nurea​​ and the surgeon Eric​​​‌ Ducasse, we aim at‌ developing reliable and automatic‌​‌ procedures for aneurysm segmentation​​ and for the prediction​​​‌ of aneurysm rupture risk.‌ Our approach exploits two‌​‌ sources of information: (i)​​ numerical simulations of blood​​​‌ flows in complex geometries,‌ based on an octree‌​‌ discretization, and (ii) computed​​ tomography angiography (CTA) data.​​​‌ Figure 4 shows the‌ force distribution on the‌​‌ walls of the abdominal​​ aorta in presence of​​​‌ an aneurysm; results are‌ obtained using a parallelized‌​‌ hierarchical Cartesian scheme based​​ on octrees.

Further information​​​‌ is given in the‌ sections dedicated to the‌​‌ new results.

Figure 4

Aneurysm simulation​​

Figure 4: force​​​‌ distribution on the walls‌ of the abdominal aorta‌​‌ in presence of an​​​‌ aneurysm.

4.4 Fluid-structure interactions​ using Eulerian non-linear elasticity​‌ models

Mathematical and numerical​​ modeling of continuum systems​​​‌ undergoing extreme regimes is​ challenging due to the​‌ presence of large deformations​​ and displacements of the​​​‌ solid part, and due​ to the strongly non-linear​‌ behavior of the fluid​​ part. At the same​​​‌ time, proper experiments of​ impact phenomena are particularly​‌ dangerous and require expensive​​ facilities, which make them​​​‌ largely impractical. For this​ reason, there is a​‌ growing interest in the​​ development of predictive models​​​‌ for impact phenomena.

In​ MEMPHIS, we rely on​‌ a fully Eulerian approach​​ based on conservation laws,​​​‌ where the different materials​ are characterized by their​‌ specific constitutive laws, to​​ address these tasks. This​​​‌ approach was introduced in​ 56 and subsequently pursued​‌ and extended in 60​​, 55, 51​​​‌, 53 and 13​. In Figure 5​‌, we show the​​ results of the numerical​​​‌ simulation of the impact​ of a copper projectile​‌ immersed in air over​​ a copper shield. Results​​​‌ are obtained using a​ fully parallel monolithic Cartesian​‌ method, based on a​​ 40002 fixed Cartesian​​​‌ grid. Simulations are performed​ on a cluster of​‌ 512 processors, and benefits​​ from the isomorphism between​​​‌ grid partitioning and processor​ topology.

Figure 5.a
 
Figure 5.b
 
Figure 5.c
  
Figure 5.d

Impact simulation

Figure​‌ 5: impact and​​ rebound of a copper​​​‌ projectile on a copper​ plate. Interface and schlieren​‌ at 50μs​​, 199μs​​​‌, 398μs​ and 710μs​‌ .

In figure 6​​, we show the​​​‌ results of a three​ dimensional simulation of a​‌ cardiac pump (LVAD, left​​ ventricule assisted device).

Figure 6

Cardiac​​​‌ pump simulation

Figure 6​: 3D numerical modeling​‌ of a cardiac pump​​ (LVAD) with an elastic​​​‌ membrane.

5 Social and​ environmental responsibility

As discussed​‌ in the previous section,​​ we are particularly interested​​​‌ in the development of​ mathematical models and numerical​‌ methods to study problems​​ related to renewable energies,​​​‌ and ultimately contribute to​ next-generation sustainable solutions for​‌ energy extraction.

5.1 Impact​​ of research results

We​​​‌ are studying two types​ of green energy extractors:​‌ wave energy converters (WECs)​​ and wind energy.

As​​​‌ regards WECs, we are​ working with the PoliTO​‌ (Torino, Italy) to model​​ the behavior of inertial​​​‌ sea wave energy converters​ (ISWEC), and we are​‌ also working with a​​ Bordeaux-based start-up for another​​​‌ device to extract energy​ from waves via an​‌ Inria-Tech project and a​​ Nouvelle-Aquitaine Regional Project submitted​​​‌ by Memphis in collaboration​ with the CARDAMOM team.​‌

As regards wind energy,​​ we focus on the​​​‌ analysis of wind turbines.​ In the past, we​‌ have supervised two PhD​​ CIFRE theses with VALOREM-Valeol,​​​‌ and are currently working​ with them in a​‌ European RISE ARIA project​​ led by Memphis. We​​​‌ also work with IFPEN​ on the aeroelastic modeling​‌ of large wind turbines​​ and the study and​​​‌ optimization of turbines farms​ in the framework of​‌ the joint laboratory Inria-IFPEN​​ with a thesis funded​​​‌ by IFPEN and a​ post-doc funded by Inria​‌ (which started in October​​ 2021).

In conjunction with​​ these activities, in collaboration​​​‌ with ANDRA (the national‌ agency for storage of‌​‌ nuclear waste), we investigated​​ the development of reduced-order​​​‌ models to allow efficient‌ and accurate simulations for‌​‌ deep geological storage planning.​​ This activity was the​​​‌ subject of the PhD‌ thesis of Giulia Sambataro‌​‌ who successfully defended her​​ PhD thesis in December​​​‌ 2022.

5.1.1 Critical Infrastructure‌ & Defense

  • EDF (Energy):‌​‌ A CIFRE thesis (A.​​ Moussaddak) was dedicated to​​​‌ the mechanical state estimation‌ of nuclear containment buildings‌​‌ (Vercors mock-up). The work​​ applied data assimilation techniques​​​‌ to identify parameters crucial‌ for the safety monitoring‌​‌ of prestressed concrete structures.​​
  • Ingeliance (Defense): This partnership​​​‌ (CIFRE thesis, M. Truel)‌ focused on Unsteady Hybrid‌​‌ Models for Fluid-Structure Interaction​​ (FSI), aiming to reduce​​​‌ computational costs for complex‌ design simulations.

6 Highlights‌​‌ of the year

  • The​​ team has organized the​​​‌ international workshop "Accurate reduced‌ Order Models". Bidart. .‌​‌
  • A publication highlighting the​​ effectiveness and robustness of​​​‌ the fluid–structure interaction schemes‌ developed by the team‌​‌ for interdisciplinary applications: Guillaume​​ Ravel, Théo Mercé, Michel​​​‌ Bergmann , Anja Knoll-Gellida,‌ Afaf Bouharguane, Sara Al‌​‌ Kassir, Angelo Iollo, and​​ Patrick J. Babin. Modeling​​​‌ zebrafish electric field pulse-induced‌ escape response reveals neuromuscular‌​‌ energetic constraints and efficient​​ body movement adaptation to​​​‌ high-viscosity fluids. iScience 28,‌ 112056, March 21, 2025.‌​‌
  • Building on the competences​​ of the MEMPHIS team​​​‌ in high-fidelity numerical methods,‌ reduced-order modeling, and hybrid‌​‌ AI/CFD approaches, the transition​​ of MEMPHIS into the​​​‌ joint Inria–Onera project-team MONHADE‌ constitutes a strategic response‌​‌ to the growing demand​​ for certified numerical simulation​​​‌ in critical sectors. With‌ the alliance with the‌​‌ French Aerospace Lab (Onera),​​ the team forms a​​​‌ focused task force targeting‌ challenges in hybrid AI/CFD‌​‌ modeling for defense and​​ aeronautics.
  • Afaf Bouharguane, member​​​‌ of the team, has‌ defended her habilitation.

7‌​‌ Latest software developments, platforms,​​ open data

7.1 Latest​​​‌ software developments

7.1.1 COCOFLOW‌

  • Keywords:
    3D, Elasticity, MPI,‌​‌ Compressible multimaterial flows
  • Functional​​ Description:
    The code is​​​‌ written in fortran 95‌ with a MPI parallelization.‌​‌ It solves equations of​​ conservation modeling 3D compressible​​​‌ flows with elastic models‌ as equation of state.‌​‌
  • Contact:
    Florian Bernard
  • Partners:​​
    CNRS, Université Bordeaux 1​​​‌

7.1.2 KOPPA

  • Name:
    Kinetic‌ Octree Parallel PolyAtomic
  • Keyword:‌​‌
    Numerical simulations
  • Functional Description:​​
    KOPPA is a C++/MPI​​​‌ numerical code solving a‌ large range of rarefied‌​‌ flows from external to​​ internal flows in 1D,​​​‌ 2D or 3D. Different‌ kind of geometries can‌​‌ be treated such as​​ moving geometries coming from​​​‌ CAO files or analytical‌ geometries. The models can‌​‌ be solved on Octree​​ grids with dynamic refinement.​​​‌
  • Contact:
    Angelo Iollo
  • Participant:‌
    an anonymous participant

7.1.3‌​‌ NaSCar3D

  • Name:
    Navier-Stokes Cartesian​​ 3D
  • Keywords:
    Navier-Stokes, Cartesian​​​‌ grid
  • Scientific Description:
    NaSCar‌ can be used to‌​‌ simulate both hydrodynamic bio-locomotion​​ as fish like swimming​​​‌ and aerodynamic flows such‌ wake generated by a‌​‌ wind turbine.
  • Functional Description:​​

    This code is devoted​​​‌ to solve 3D-flows in‌ around moving and deformable‌​‌ bodies. The incompressible Navier-Stokes​​ equations are solved on​​​‌ fixed grids, and the‌ bodies are taken into‌​‌ account thanks to penalization​​​‌ and/or immersed boundary methods.​ The interface between the​‌ fluid and the bodies​​ is tracked with a​​​‌ level set function or​ in a Lagrangian way.​‌ The numerical code is​​ fully second order (time​​​‌ and space). The numerical​ method is based on​‌ projection schemes of Chorin-Temam's​​ type. The code is​​​‌ written in C language​ and use Petsc library​‌ for the resolution of​​ large linear systems in​​​‌ parallel.

    NaSCar can be​ used to simulate both​‌ hydrodynamic bio-locomotion as fish​​ like swimming and aerodynamic​​​‌ flows such wake generated​ by a wind turbine.​‌

  • URL:
  • Contact:
    Michel​​ Bergmann
  • Participant:
    an anonymous​​​‌ participant

7.1.4 NS-penal

  • Name:​
    Navier-Stokes-penalization
  • Keywords:
    3D, Incompressible​‌ flows, 2D
  • Functional Description:​​
    The software can be​​​‌ used as a black​ box with the help​‌ of a data file​​ if the obstacle is​​​‌ already proposed. For new​ geometries the user has​‌ to define them. It​​ can be used with​​​‌ several boundary conditions (Dirichlet,​ Neumann, periodic) and for​‌ a wide range of​​ Reynolds numbers.
  • Contact:
    Charles-Henri​​​‌ Bruneau
  • Partner:
    Université de​ Bordeaux

7.1.5 HiWind

  • Keyword:​‌
    Simulation
  • Functional Description:
    Hiwind​​ is a software that​​​‌ allows to model in​ 2D and 3D the​‌ effects of air flow​​ on a wind turbine​​​‌ blade (moving solid or​ elastic structures), and to​‌ simulate numerically their interactions.​​ Hiwind also allows to​​​‌ model and characterize the​ abnormal behavior to warn​‌ about a potential weakening​​ of the structure. Hiwind​​​‌ is a "drag and​ drop" solution (automated meshing​‌ phase), massively parallel, and​​ uses adaptive meshing.
  • Contact:​​​‌
    Angelo Iollo
  • Partner:
    Valeol​

7.1.6 NEOS

  • Functional Description:​‌
    NEOS is a software​​ framework for numerical modeling​​​‌ of multiphysical problems on​ hierarchical Cartesian meshes (quadtree​‌ in 2D and octree​​ in 3D). It is​​​‌ mainly based on the​ bitpit library (https://optimad.github.io/bitpit/). NEOS​‌ provides : - the​​ creation and parallel management​​​‌ of hierarchical Cartesian meshes​ (2D quadtree or 3D​‌ octree) - global or​​ local mesh refinement (based​​​‌ on a distance of​ levelset or other physical​‌ criteria) - the management​​ of several moving geometries​​​‌ in an analytical or​ explicit form (STL files​‌ or others) - the​​ calculation of geometries levelsets​​​‌ at any point of​ the mesh - 2D/3D​‌ differential operators of (gradient,​​ laplacian, hessian, ...) -​​​‌ various 2D/3D interpolators (bilinear,​ radial basis functions RBF)​‌ - an API for​​ solvers (currently with PETSC)​​​‌ - a complete Python3​ interface
  • Contact:
    Michel Bergmann​‌

8 New results

8.1​​ Nonlinear approximation methods based​​​‌ on coordinate transformations

Participants:​ Angelo Iollo, Jon​‌ Labatut, Tommaso Taddei​​, Ishak Tifouti,​​​‌ Mathias Truel, Michel​ Bergmann.

A significant​‌ limitation of MOR techniques​​ that rely on linear​​​‌ approximation spaces is their​ inability to effectively handle​‌ parameter-dependent sharp gradients, which​​ naturally arise in the​​​‌ solutions to advection-dominated problems.​ This inadequacy of linear​‌ approximations has spurred the​​ development of nonlinear methods.​​​‌ Among these, nonlinear approaches​ based on coordinate transformations​‌ have demonstrated their effectiveness​​ across a wide range​​​‌ of problems in computational​ mechanics. These techniques rely​‌ on a registration procedure​​ to find a parametric​​ spatio(-temporal) transformation that improves​​​‌ the linear compressibility of‌ the solution set.

The‌​‌ development of registration techniques​​ for MOR has been​​​‌ a major focus of‌ the team's research. We‌​‌ refer to the HDR​​ thesis of Tommaso Taddei​​​‌ for a recent review‌ of the ongoing efforts‌​‌ on the subject 23​​. In the past​​​‌ year, three significant advances‌ have been achieved in‌​‌ this direction.

  1. Jon Labatut​​ 35 developed a novel​​​‌ registration framework based on‌ parametric vector flows and‌​‌ coupled the approach with​​ the convex displacement interpolation​​​‌ method of 14 for‌ two-dimensional and three-dimensional aerodynamic‌​‌ problems. Jon Labatut defended​​ his PhD thesis in​​​‌ November 2025 40;‌ we are currently working‌​‌ on the submission of​​ two papers from the​​​‌ thesis. Figure 7 shows‌ select numerical results from‌​‌ Labatut's thesis for a​​ three-dimensional viscous problem.
  2. Iollo​​​‌ and Taddei proposed a‌ new registration method in‌​‌ bounded domains using Fokker​​ Planck equation 15.​​​‌ This paper has led‌ to an ongoing collaboration‌​‌ with Giovanni Russo (University​​ of Catania) and Klaas​​​‌ Wilhems (KU Leuven) on‌ the development of specialized‌​‌ methods for the Fokker​​ Planck equation in bounded​​​‌ domains.
  3. Tifouti 34 developed‌ a registration-based MOR framework‌​‌ with local reduced-order bases​​ that extends the work​​​‌ in 2 to deal‌ with shock-topology changes. Ishak‌​‌ Tifouti defended his PhD​​ thesis in November 2025​​​‌ 24; we expect‌ to submit one paper‌​‌ based on his work​​ in 2026.
  4. Mathias Truel​​​‌ mainly worked on a‌ non-linear interpolation technique based‌​‌ on mappings. A mapping​​ is defined using Free-Form​​​‌ Deformation (FFD) and is‌ parametrized by control points.‌​‌ The displacement of control​​ points is tuned via​​​‌ the minimization of an‌ objective function. Implementation using‌​‌ the JAX library allows​​ the use of a​​​‌ fast L-BFGS solver. In‌ Figure 8, a‌​‌ simple registration case between​​ u0 and u​​​‌1 is demonstrated. The‌ domain is divided into‌​‌ two subdomains and two​​ FFD formulations are used.​​​‌ The control points for‌ the first (red circles)‌​‌ and second (blue squares)​​ FFD are depicted. The​​​‌ yellow crosses are synchronization‌ points, where the two‌​‌ mappings are equal. Overall,​​ four mappings are optimized.​​​‌ Two for the direction‌ 01 and‌​‌ two for 1→​​0. After minimizing​​​‌ the objective function, two‌ interpolations are constructed, one‌​‌ where u1 is​​ deformed into u0​​​‌ and the opposite. Displacements‌ of control points and‌​‌ synchronization points are also​​ shown. To easily visualize​​​‌ the mappings in the‌ domains, a checkerboard pattern‌​‌ is deformed.
 

Application of​​ the convex displacement interpolation​​​‌ to an ONERA M6‌ wing in the transonic‌​‌ viscous regime for varying​​ angle of attack. Left:​​​‌ density over the wing.‌ Right: comparison of density‌​‌ residuals convergence with different​​ initialization of the full-order​​​‌ model (CDI=convex displacement interpolation;‌ CI=convex interpolation; P0=piecewise-constant DG‌​‌ solution).

Application of the​​ convex displacement interpolation to​​​‌ an ONERA M6 wing‌ in the transonic viscous‌​‌ regime for varying angle​​ of attack. Left: density​​​‌ over the wing. Right:‌ comparison of density residuals‌​‌ convergence with different initialization​​​‌ of the full-order model​ (CDI=convex displacement interpolation; CI=convex​‌ interpolation; P0=piecewise-constant DG solution).​​

Figure 8

Example of the FFD​​​‌ mapping applied to a​ translated square.

8.2 Collocation-based​‌ reduced order models: analysis​​ and applications

Participants: Michel​​​‌ Bergmann, Michele Giuliano​ Carlino, Elise Declerck​‌, Alessia Del Grosso​​, Angelo Iollo,​​​‌ Marc-Olivier Potin.

The​ primary methodological investigation centers​‌ on collocation strategies in​​ Model Order Reduction (MOR)​​​‌ 27, designed to​ enhance the efficiency of​‌ the online-offline paradigm. Unlike​​ standard pROMs where solutions​​​‌ are projected onto a​ reduced basis, this approach​‌ solves governing equations at​​ a sparse set of​​​‌ optimal collocation points. The​ research utilizes the Non-Negative​‌ Least Square (NNLS) algorithm​​ to identify a minimal​​​‌ set of collocation points​ (cells) and associated positive​‌ weights during the offline​​ phase. This significantly reduces​​​‌ computational cost as the​ number of collocation points​‌ is much smaller than​​ the total discretization cells.​​​‌

In the most recent​ developments, not published yet,​‌ we analyze two distinct​​ implementations:

  1. Collocated projection-based ROM​​​‌ (cpROM): This method computes​ the solution approximation in​‌ all cells using the​​ reduced ansatz. Theoretically, it​​​‌ is the closest to​ the classic pROM; if​‌ all discretized cells are​​ used as collocation points,​​​‌ cpROM and pROM coincide.​
  2. Collocation-based ROM (cROM): This​‌ method applies the reduced​​ ansatz only in cells​​​‌ neighboring the collocation points.​ It differs significantly in​‌ theory; if all cells​​ are used, the cROM​​​‌ coincides with the HF​ discretization.

Current work establishes​‌ theoretical foundations for these​​ methods. Specifically, for the​​​‌ cROM case, an equivalence​ result analogous to the​‌ Lax-Richtmyer theorem 59 is​​ derived, where stability and​​​‌ consistency imply convergence.

Structure-preserving​ cROM.

A critical challenge​‌ in MOR is ensuring​​ that reduced models retain​​​‌ the essential physical properties​ of the HF source​‌ model. This line of​​ research aims to develop​​​‌ structure-preserving ROMs that strictly​ satisfy physical constraints. We​‌ are currently investigating the​​ shallow water system with​​​‌ wet-dry fronts. In particular,​ Giorgio Musso, during his​‌ master thesis, implemented a​​ novel transformation approach to​​​‌ strictly preserve the non-negativity​ of water height during​‌ simulations, a property often​​ violated by classical projection​​​‌ methods. Giorgio will continue​ working on these topics​‌ during his PhD that​​ has recently started (supervised​​​‌ by A. Del Grosso​ in collaboration with C.​‌ Fiorini of CNAM).

Implicit-explicit​​ (IMEX) schemes for cROM.​​​‌

We extended the collocation-based​ methodology to IMEX time​‌ integrators. The explicit contribution​​ is treated via projection/prolongation​​​‌ of the reduced solution​ onto cells within the​‌ collocation stencils. The implicit​​ stage involves solving a​​​‌ system Au=​b of size N​‌. By pre-multiplying by​​ a Boolean masking matrix​​​‌ MN​c×N and​‌ post-multiplying by the prolongation​​ operator Pℝ​​​‌N×Nc​, we obtain a​‌ reduced implicit system:

M​​ A P u =​​​‌ b c

This work​ is conducted in collaboration​‌ with CNRS researcher Walter​​ Boscheri and Beatrice Battisti​​​‌ (Université Savoie Mont Blanc).​ To handle physical models​‌ with non-linear diffusion coefficients,​​ we are currently investigating​​ hyper-reduction strategies (specifically gappy​​​‌ POD) to approximate algebraic‌ operators without full domain‌​‌ assembly.

Neural Network Correction​​ for Explicit Schemes.

To​​​‌ enhance the accuracy of‌ cROMs, we introduced a‌​‌ hybrid correction strategy 50​​. A neural network​​​‌ is trained to learn‌ a nonlinear decoder that‌​‌ accounts for solution features​​ lying in the orthogonal​​​‌ complement of the Reduced‌ Basis. At each time‌​‌ step, the standard cROM​​ prediction is enriched by​​​‌ a nonlinear correction term.‌ The network uses the‌​‌ orthogonal residual—obtained by projecting​​ high-fidelity snapshots onto the​​​‌ complement of the reduced‌ space—as an input feature.‌​‌ This approach preserves the​​ non-intrusiveness of the collocation​​​‌ framework while capturing complex‌ nonlinear behaviors that escape‌​‌ linear subspace approximations. Preliminary​​ results indicate significant accuracy​​​‌ improvements in multiscale and‌ strongly nonlinear regimes. This‌​‌ work is ongoing.

CFD-based​​ reduced-order modeling of a​​​‌ turbine stage for parametric‌ optimization.

In order to‌​‌ approach the problem, we​​ first modelize the air​​​‌ flow using 1D Euler‌ equations in a tube.‌​‌ These equations are solved​​ numerically in python using​​​‌ finite volume schemes.

Figure 9

Physical‌ variables density ρ,‌​‌ pressure P, vitesse​​ U, Mach M​​​‌, predicted by component-based‌ ROM (blue) and high-fidelity‌​‌ (orange)

Then we built​​ two types of reduced​​​‌ order model (ROM) of‌ this high fidelity model‌​‌ : Petrov-Galerkin projection-based reduced​​ order model (pROM) and​​​‌ collocation-based reduced order model‌ (cROM) The equations are‌​‌ solved in a subspace​​ determined with proper orthogonal​​​‌ decomposition (POD). In the‌ pROM, the non-linear term‌​‌ is hyper-reduced using the​​ NNLS algorithm to prevent​​​‌ a computational bottleneck. The‌ cROM uses NNLS and‌​‌ the POD to determine​​ a subset of points​​​‌ where the high-fidelity volume‌ scheme is solved. Domain‌​‌ decomposition consists in dividing​​ the domain into subdomains.​​​‌ Each subdomain has its‌ own ROM, allowing multifidelity‌​‌ simulation. We use such​​ simulations to train a​​​‌ model starting from a‌ coarse grid then using‌​‌ a finer grid and​​ full-order model on each​​​‌ subdomain with a MOR‌ on the other. Repeating‌​‌ these steps, we build​​ a component-based ROM on​​​‌ the domain for the‌ finer grid (see Figure‌​‌ 9).

Optimal Domain​​ Decomposition in Multifidelity Modeling​​​‌ for Uncertain Geometries in‌ Fluid-Structure Interaction.

In the‌​‌ PhD thesis of Marc-Olivier​​ Potin, we develop a​​​‌ numerical hybridization architecture based‌ on the multi-fidelity paradigm.‌​‌ This approach aims to​​ exploit the plurality of​​​‌ industrial flows: while critical‌ areas (where strong nonlinearities‌​‌ and transient phenomena occur)​​ require high-fidelity resolution (HFM),​​​‌ large portions of the‌ fluid domain exhibit more‌​‌ regular dynamics that can​​ be effectively described by​​​‌ reduced-order models (ROMs). Figure‌ 10 illustrates part of‌​‌ the results of the​​ hybrid multi-fidelity scheme applied​​​‌ to 1D Euler equations‌ in a Laval nozzle‌​‌ configuration (overset mesh). This​​ test case, representative of​​​‌ transonic compressible flows with‌ shock wave, highlights the‌​‌ behavior of the hyper-reduction​​ algorithm (cMOR) on the​​​‌ background grid. The results‌ demonstrate a direct correlation‌​‌ between the selection tolerance​​ ϵ and the fidelity​​​‌ of the solution. Analysis‌ of the cost/accuracy trade-off‌​‌ reveals that it is​​​‌ possible to achieve a​ relative space-time error of​‌ less than 2%, while​​ reducing computation time by​​​‌ up to 55%. This​ validation on 1D cases​‌ provides the proof of​​ concept needed to extend​​​‌ this procedures to complex​ 2D industrial geometries.

Figure 10

Density​‌ profiles along the Laval​​ nozzle at steady state.​​​‌ Comparison of solutions obtained​ for different settings of​‌ the cMOR hyper-reduced model.​​

8.2.1 Component-based model reduction​​​‌ of complex systems

Participants:​ Tommaso Taddei, Lei​‌ Zang.

“Classical” (monolithic)​​ MOR methods rely on​​​‌ three fundamental assumptions: first,​ the solution is defined​‌ over a parameter-independent spatial​​ domain; second, it is​​​‌ computationally feasible to solve​ the full-order model (FOM)​‌ for several parameter values​​ during the offline stage;​​​‌ third, parameter variations induce​ changes in the solution​‌ field that can be​​ captured by a global​​​‌ (in space and in​ parameter) low-dimensional approximation. Classical​‌ MOR methods are hence​​ ill-suited to deal with​​​‌ problems with parameter-induced topology​ changes.

Component-based (or localized)​‌ model order reduction (CB-MOR)​​ techniques combine approaches from​​​‌ model reduction and domain​ decomposition (DD) to overcome​‌ or significantly mitigate limitations​​ of monolithic strategies. CB-MOR​​​‌ techniques are based on​ the introduction of a​‌ library of archetype components​​ and are heavily inspired​​​‌ by the extensive literature​ on component mode synthesis​‌ (CMS) and dynamic substructuring.​​ Research on CB-MOR has​​​‌ reached a mature stage​ for linear problems; however,​‌ extending these techniques to​​ nonlinear and time-dependent regimes​​​‌ remains an extremely challenging​ task.

In 2025, Tommaso​‌ Taddei and collaborators worked​​ on the development of​​​‌ component-based model reduction techniques​ for incompressible flows. In​‌ more detail, in 65​​, they extended the​​​‌ method of 63 to​ fluid structure interaction problems​‌ that feature laminar incompressible​​ flows with hyper-elastic structures.​​​‌ More recently, the same​ authors have considered a​‌ different coupling strategy that​​ is provably energy stable​​​‌ at the semi-discrete level​ and have shown that​‌ the use of high-order​​ implicit Runge Kutta methods​​​‌ leads to dramatic improvements​ in the long-term stability​‌ of the reduced-order model​​ 64.

Figures 11​​​‌ and 12 show select​ results from 64 for​‌ the Turek benchmark (FSI3,​​ 67).

Figure 11​​​‌ shows three snapshots of​ the horizontal velocity field​‌ at three time instants​​ t=32,​​​‌35,38s​ for a representative parameter​‌ value: the plots illustrate​​ the formation of a​​​‌ periodic vortex street downstream​ of the cylinder and​‌ the associated oscillatory motion​​ of the beam.

Figure 11.a
  
Figure 11.b
  
Figure 11.c

Turek;​​​‌ x-velocity field at 3​ time instants (t​‌=32-35-38).

Figures 12​​(a) and (b) show​​​‌ the spectra of drag​ and lifted forces obtained​‌ by ROMs for different​​ POD tolerances at two​​​‌ representative test points: we​ observe that the CB-ROM​‌ is effective to approximate​​ the spectra of the​​​‌ force on the structure​ for out-of-sample configurations. Figure​‌ 12(c) shows the​​ number of retained POD​​​‌ modes for velocity (​nu), pressure​‌ (np),​​ and displacement (n​​​‌s) — the​ method also includes control​‌ variables associated with the​​ displacement at the interface​​ nc. We​​​‌ notice that the number‌ of modes that are‌​‌ required to reach an​​ acceptable accuracy is extremely​​​‌ large: this result clearly‌ shows the need for‌​‌ nonlinear approximation methods.

Figure 12.a
  
Figure 12.b
  
Figure 12.c

Turek​​ benchmark. (Fx)-(Fy)-Number of modes.​​​‌ Comparison of spectra of‌ drag and lifted forces‌​‌ obtained by ROMs for​​ different POD tolerances at​​​‌ two representative test points.‌ (c) ROM errors and‌​‌ number of modes versus​​ POD tolerance.

8.3 Reduced-Order​​​‌ Modeling with Active Subspace‌ Closure

Participants: Angelo Iollo‌​‌, Tommaso Taddei,​​ Alexis Valls.

This​​​‌ activity focuses on the‌ development of data-driven closure‌​‌ strategies for reduced-order models​​ (ROMs) of nonlinear, advection-dominated​​​‌ dynamical systems. The work‌ is illustrated on the‌​‌ Kuramoto–Sivashinsky equation, a canonical​​ model sharing structural similarities​​​‌ with the Navier–Stokes equations‌ while remaining computationally affordable‌​‌ for extensive high-fidelity simulations.​​

Starting from a Proper​​​‌ Orthogonal Decomposition (POD)–Galerkin projection,‌ the system dynamics are‌​‌ decomposed into resolved large-scale​​ modes and unresolved small-scale​​​‌ modes. Standard Galerkin ROMs‌ fail to accurately reproduce‌​‌ the long-term dynamics due​​ to the neglected influence​​​‌ of unresolved scales, which‌ motivates the introduction of‌​‌ closure terms.

A first​​ approach considers a Markovian,​​​‌ memoryless closure, where the‌ effect of unresolved modes‌​‌ is approximated by parametric​​ correction terms depending only​​​‌ on the resolved variables.‌ These parameters are identified‌​‌ from data using least-squares​​ regression on high-fidelity snapshots.​​​‌ While this approach improves‌ short-term accuracy, it requires‌​‌ a large number of​​ learned parameters and offers​​​‌ limited interpretability.

To address‌ these limitations, a novel‌​‌ closure strategy based on​​ the concept of active​​​‌ subspaces is introduced. The‌ key idea is to‌​‌ identify low-dimensional directions in​​ the unresolved space that​​​‌ have the strongest influence‌ on the closure term.‌​‌ This is achieved by​​ analyzing the sensitivity of​​​‌ the closure with respect‌ to unresolved variables and‌​‌ computing the dominant eigenvectors​​ of an associated averaged​​​‌ gradient covariance operator. The‌ resulting active modes define‌​‌ a reduced basis for​​ the unresolved dynamics, leading​​​‌ to a compact and‌ physically interpretable closure model.‌​‌

Preliminary results indicate that​​ only a small number​​​‌ of active directions are‌ sufficient to capture the‌​‌ dominant interactions between resolved​​ and unresolved scales, supporting​​​‌ the relevance of the‌ proposed approach. Ongoing work‌​‌ focuses on coupling the​​ reduced active variables with​​​‌ the resolved dynamics through‌ consistent evolution equations, paving‌​‌ the way toward efficient​​ and robust non-intrusive ROM​​​‌ closures for complex fluid‌ systems.

8.4 Output reduction:‌​‌ Clustered active subspaces

Participants:​​ Michel Bergmann, Maxime​​​‌ Chapron.

Aerodynamic shape‌ optimization often involves navigating‌​‌ extremely high-dimensional design spaces​​ and relying on computationally​​​‌ expensive simulations, making standard‌ surrogate-based optimization methods difficult‌​‌ to apply because they​​ suffer from the curse​​​‌ of dimensionality. A widely‌ used strategy to overcome‌​‌ this challenge is dimension​​ reduction, which seeks to​​​‌ identify a smaller set‌ of directions that most‌​‌ strongly influence the objective​​ function. One prominent technique,​​​‌ known as Active Subspaces‌ (AS), uses gradient information‌​‌ to uncover linear combinations​​ of input parameters that​​​‌ explain the dominant variations‌ in system performance, allowing‌​‌ surrogate models such as​​​‌ Kriging to be trained​ within a far lower-dimensional​‌ space while maintaining accuracy.​​

Yet, global dimension reduction​​​‌ can be insufficient when​ dealing with complex, highly​‌ nonlinear, or multimodal response​​ surfaces, since no single​​​‌ reduced representation can capture​ all relevant behaviors across​‌ the entire design domain.​​ To address this limitation,​​​‌ the Clustered Active Subspaces​ (CAS) framework adopts a​‌ divide-and-conquer methodology:

  • The design​​ space is first partitioned​​​‌ using clustering algorithms such​ as Gaussian Mixture Models,​‌ which identify regions of​​ similar functional behavior rather​​​‌ than grouping points simply​ by geometric distance.
  • Each​‌ cluster is then assigned​​ its own local active​​​‌ subspace and its corresponding​ local surrogate model.
  • These​‌ local predictions are combined​​ through a Mixture-of-Experts formulation​​​‌ to construct a coherent​ global model.

This approach​‌ improves robustness, scalability, and​​ predictive accuracy, particularly in​​​‌ complex aerodynamic settings. Within​ Bayesian Optimization, performing the​‌ search in the reduced​​ space greatly simplifies the​​​‌ maximization of acquisition functions.​ Two additional steps are​‌ essential for this integration:​​ accurately defining the boundaries​​​‌ of the reduced domain​ (which takes the form​‌ of a zonotope) to​​ avoid unreliable extrapolation; and​​​‌ mapping optimized points from​ the reduced space back​‌ into the full-dimensional design​​ space.

This work has​​​‌ been carried out with​ ONERA during the thesis​‌ of Maxime Chapron, also​​ presented at several conferences​​​‌ 12, 11.​

8.5 Local reduction: Data-Driven​‌ Wall Modeling for Industrial​​ RANS Simulations

Participants: Michel​​​‌ Bergmann, Michele Romanelli​.

By enabling accurate​‌ predictions of wall shear​​ stress without resolving the​​​‌ near-wall viscous sublayer, data-driven​ wall models provide a​‌ powerful form of local​​ model reduction that allows​​​‌ the use of significantly​ coarser meshes in the​‌ vicinity of the wall​​ while maintaining high fidelity​​​‌ in RANS simulations. During​ the PhD thesis of​‌ Michele Romanelli 22,​​ two works 20,​​​‌ 21 advance the development​ of accurate and computationally​‌ efficient data-driven wall models​​ for turbulent boundary layers​​​‌ subjected to arbitrary pressure​ gradients.

  • Implicit Framework: The​‌ first study 20 introduces​​ a general machine-learning framework​​​‌ that replaces traditional analytical​ wall laws with a​‌ non-parametric model constructed from​​ high-fidelity data. By reformulating​​​‌ the wall boundary condition​ as a Dirichlet-to-Neumann operator​‌ applied at a fixed​​ distance from the wall​​​‌ (typically y+≈​30–50), a neural​‌ network predicts instantaneous wall​​ shear stress. While significantly​​​‌ outperforming classical formulations in​ regions of strong acceleration​‌ or separation, this approach​​ relies on an iterative​​​‌ recovery of skin-friction, adding​ computational overhead.
  • Explicit Framework:​‌ The second contribution 21​​ resolves this bottleneck by​​​‌ proposing a fully explicit​ data-driven wall model. A​‌ dedicated neural network directly​​ outputs the magnitude and​​​‌ direction of the wall​ shear stress from an​‌ enriched set of non-dimensional​​ local inputs (including velocity-profile​​​‌ samples and pressure-gradient components).​ This explicit formulation removes​‌ the need for any​​ iterative solver, yielding one​​​‌ to two orders of​ magnitude speedup while preserving​‌ essentially identical predictive accuracy.​​

Together, these developments establish​​​‌ a coherent framework for​ data-driven wall modeling, demonstrating​‌ that such models are​​ mature enough for deployment​​ in aerodynamic design and​​​‌ uncertainty-quantification workflows.

8.6 Numerical‌ Schemes for Multiphysics

Participants:‌​‌ Alessia Del Grosso,​​ Angelo Iollo.

Non-conservative​​​‌ and Relaxation Schemes for‌ Monolithic Elastic Modeling.

We‌​‌ investigated the numerical treatment​​ of the evolution equation​​​‌ for gradient deformation in‌ solid mechanics. Traditional conservative‌​‌ approaches represent this variable​​ using the gradient of​​​‌ backward characteristics. While this‌ ensures conservation and captures‌​‌ discontinuities, it significantly increases​​ the system size (four​​​‌ equations in 2D and‌ nine in 3D, compared‌​‌ to two and three,​​ respectively) and complicates the​​​‌ preservation of the irrotational‌ property. To address this,‌​‌ we proposed a non-conservative​​ formulation by directly integrating​​​‌ the transport equation for‌ the backward characteristics. This‌​‌ approach reduces the system​​ size and automatically preserves​​​‌ the involutive constraint to‌ machine precision, whereas standard‌​‌ Lax-Friedrichs (LF) methods typically​​ exhibit errors of order​​​‌ 10-2.‌ However, simulating non-conservative models‌​‌ with discontinuous solutions presents​​ stability challenges, specifically regarding​​​‌ path-dependence 61. To‌ ensure consistency with weak‌​‌ solutions, we developed a​​ simplified approach based on​​​‌ the Jin-Xin relaxation strategy‌ 52. As illustrated‌​‌ in Figure 13,​​ the proposed relaxation method​​​‌ yields results analogous to‌ the reference conservative LF‌​‌ method while maintaining a​​ reduced computational footprint.

 
 

Density​​​‌ solution for the 2D‌ Riemann problem in a‌​‌ copper domain (20 contour​​ lines). Top Left: Reference​​​‌ conservative Lax-Friedrichs (LF) solution.‌ Top Right: Explicit non-conservative‌​‌ relaxation scheme. Bottom Left:​​ Non-conservative IMEX scheme with​​​‌ explicit time step. Bottom‌ Right: IMEX scheme with‌​‌ a time step 1000​​× larger than the​​​‌ explicit limit.

Implicit-explicit strategies‌ for multi-scale flows.

A‌​‌ significant challenge in fluid-structure​​ interaction is the disparity​​​‌ in wave speeds, particularly‌ in the subsonic regime‌​‌ (M<1​​) where solid waves​​​‌ are significantly slower than‌ fluid waves. The classic‌​‌ Courant-Friedrichs-Lewy (CFL) condition is​​ driven by the fast​​​‌ waves, leading to excessive‌ diffusion in the approximation‌​‌ of slow (solid) waves.​​

To mitigate this, we​​​‌ applied IMEX strategies inspired‌ by 66, 49‌​‌. We treat the​​ fast waves implicitly to​​​‌ bypass the acoustic CFL‌ restriction, while keeping other‌​‌ terms explicit.

  • Lagrange-Projection methods:​​ During the master internship​​​‌ of Sofia Curto, we‌ exploited implicit-explicit Lagrange-Projection (LP)‌​‌ methods 57. This​​ approach allows for a​​​‌ natural decomposition of wave‌ speeds and was successfully‌​‌ applied to the monolithic​​ hyper-elastic model.
  • Implicit all-Mach​​​‌ relaxation: We developed an‌ implicit relaxation scheme for‌​‌ the simulation of compressible​​ flows across all Mach​​​‌ number regimes based on‌ the Jin-Xin relaxation approach.‌​‌ The scheme is characterized​​ by its simplicity and​​​‌ effectiveness: thanks to the‌ linearity of the flux‌​‌ in the relaxation system,​​ the time-semi discrete scheme​​​‌ can be reformulated into‌ linear decoupled elliptic equations,‌​‌ resulting in the same​​ number of unknowns as​​​‌ the original system. To‌ ensure correct numerical diffusion‌​‌ in all regimes, a​​ convex combination of upwind​​​‌ and centered fluxes is‌ applied. This method was‌​‌ validated on non-linear elasticity​​ models, as well as​​​‌ gas and fluid flow‌ simulations, demonstrating accuracy in‌​‌ approximating material waves across​​​‌ different Mach regimes.
  • Performance:​ As shown in Figure​‌ 13 (bottom right), the​​ IMEX approach correctly captures​​​‌ material waves even when​ using a time step​‌ 1000 times larger than​​ the explicit stability limit.​​​‌

8.6.1 High-order ADER-DG for​ Advection-Diffusion and Navier-Stokes

Participants:​‌ Afaf Bouharguane, Angelo​​ Iollo, Alexis Tardieu​​​‌.

In parallel to​ solid mechanics, we investigated​‌ high-order schemes for fluid​​ flows characterized by strongly​​​‌ varying physical parameters across​ internal interfaces. Classical body-fitted​‌ meshes, while precise, are​​ computationally expensive to generate​​​‌ for moving interfaces and​ complicate parallel partitioning.

To​‌ address this, our research​​ has focused on non-conforming​​​‌ hierarchical meshes (quadtrees or​ octrees), which offer efficient​‌ adaptation and parallelization. Previous​​ work in the team​​​‌ (Raeli, Taymans, Fondanèche) utilized​ Finite Difference and Finite​‌ Volume schemes on such​​ grids; however, the necessity​​​‌ of wide stencils for​ polynomial reconstruction limited both​‌ parallel efficiency and the​​ achievable order of accuracy.​​​‌ Conversely, recent ADER strategies​ on Chimera grids (Carlino)​‌ achieved high-order temporal accuracy​​ but suffered from precision​​​‌ loss in mesh overlap​ zones.

Consequently, we developed​‌ a new Discontinuous Galerkin​​ (DG) scheme combined with​​​‌ an ADER time integration​ approach. By leveraging a​‌ compact stencil and an​​ arbitrary high-order polynomial representation,​​​‌ this method overcomes the​ limitations of previous hierarchical​‌ solvers.

  • Methodology: We established​​ the optimal performance compromise​​​‌ by analyzing both penalization​ and relaxation approaches.
  • Validation​‌ and Extension: The scheme​​ was validated on the​​​‌ non-linear advection-diffusion equation and​ successfully extended to the​‌ simulation of incompressible flows​​ via the Navier-Stokes equations.​​​‌
  • Perspectives: This work lays​ the foundation for compact,​‌ high-precision solvers on hybrid​​ Chimera/quadtree grids, targeting the​​​‌ realistic simulation of boundary​ layers in aerodynamics, such​‌ as flows around airfoils​​ and turbine blades.

Alexis​​​‌ Tardieu has defended his​ PhD in December 2025​‌ 43 and he published​​ two papers.

8.7 Biological​​​‌ Fluid Dynamics and Locomotion​

Participants: Michel Bergmann,​‌ Angelo Iollo, Karl​​ Maroun.

This research​​​‌ axis leverages high-performance computational​ fluid dynamics (CFD) to​‌ model flow around immersed,​​ mobile, and deformable bodies.​​​‌ The common methodological denominator​ is the use of​‌ penalty methods and Cartesian​​ grid solvers to handle​​​‌ complex fluid-structure interactions (FSI).​

Data-Driven Simulation of Zebrafish​‌ Locomotion.

The zebrafish is​​ a critical model for​​​‌ studying locomotor diseases. We​ developed a numerical model​‌ driven by experimental data​​ to simulate the escape​​​‌ swim of the zebrafish​ eleuthero-embryo 19. The​‌ solver couples the incompressible​​ Navier–Stokes equations with Newton's​​​‌ laws, using a level-set​ function to represent the​‌ body implicitly. To ensure​​ high fidelity, deformation kinematics​​​‌ were estimated directly from​ experimental videos using Procrustes​‌ analysis, and the morphology​​ was reconstructed in 3D​​​‌ by tracking Lagrangian markers.​ This framework allowed for​‌ the accurate in silico​​ reproduction of the stereotyped​​​‌ escape response (C-bend, counter-bend,​ and cyclic swimming) and​‌ enabled a study on​​ the Cost of Transport​​​‌ (CoT). Results indicated a​ linear response in transport​‌ cost associated with constant​​ energy expenditure, independent of​​​‌ fluid viscosity. Numerical results​ are obtained with the​‌ in-house software NaSCar.

Multiphysics​​ Modeling of Aquatic Maneuvers.​​

We extended the framework​​​‌ to multiphysics scenarios, such‌ as the self-propelled dolphin‌​‌ jump (Figure 14).​​ The model utilizes a​​​‌ fictitious domain approach with‌ Volume Penalization (VP) for‌​‌ the solid body and​​ the Continuous Surface Force​​​‌ (CSF) method for the‌ air-water interface 8.‌​‌

Figure 14

Numerical simulation of a​​ self-propelled dolphin jump, illustrating​​​‌ the interaction between the‌ dolphin body, water, and‌​‌ air.

The geometry, based​​ on Lagenorhynchus obliquidens,​​​‌ follows thunniform deformation laws‌ while global motions are‌​‌ computed dynamically. This approach​​ successfully captures the complex​​​‌ interaction between the swimmer‌ and the free surface.‌​‌ Numerical results are obtained​​ with the in-house software​​​‌ NaSCar.

Optimization and Control‌ of Undulatory Swimming.

In‌​‌ the context of the​​ ANR project DRAGON2, we​​​‌ developed a framework for‌ the optimal control of‌​‌ swimming 17. To​​ mitigate the computational cost​​​‌ of high-fidelity simulations, Sparse‌ Identification of Nonlinear Dynamics‌​‌ (SINDy) was employed to​​ generate surrogate models. These​​​‌ models facilitated the solution‌ of control problems, including‌​‌ velocity tracking via Model​​ Predictive Control (MPC) and​​​‌ the minimization of the‌ Cost of Transport (CoT).‌​‌ The optimization yielded a​​ "burst-and-coast" strategy, validating the​​​‌ energy efficiency of intermittent‌ swimming behaviors. Numerical results‌​‌ are obtained with the​​ in-house software NaSCar.

Collective​​​‌ Dynamics of Microswimmers.

In‌ collaboration with LOMA, we‌​‌ investigated the behavior of​​ artificial swimmers in confined​​​‌ environments (Figure 15).‌ The numerical framework integrated‌​‌ penalization methods with short-range​​ contact forces (lubrication and​​​‌ collision) to accurately simulate‌ collective dynamics 28.‌​‌

Figure 15

Direct numerical simulation of​​ artificial swimmers in a​​​‌ confined impermeable arena, showing‌ spatial distribution and flow‌​‌ structures.

The simulations successfully​​ reproduced experimental observations, such​​​‌ as wall accumulation and‌ the reduction of mean‌​‌ velocity with increasing group​​ size, elucidating the role​​​‌ of boundary properties in‌ shaping wake structures. Numerical‌​‌ results are obtained with​​ the in-house software NaSCar.​​​‌

8.8 Multi-fidelity multi-scale numerical‌ modeling of wave energy‌​‌ converter farms

Participants: Beatrice​​ Battisti, Michel Bergmann​​​‌.

High-fidelity three-dimensional models‌ provide accurate results for‌​‌ wave energy converters (WECs)​​ simulations, but are too​​​‌ computationally expensive. Projection-based model‌ order reduction techniques based‌​‌ on Proper Orthogonal Decomposition​​ (POD) have demonstrated effectiveness​​​‌ in simulating single-phase flows,‌ but encounter stability challenges‌​‌ with multiphase flows. Tests​​ presented in the thesis​​​‌ indicate that classical methods‌ bypassing full-order models are‌​‌ not viable in this​​ context. A multi-fidelity, Galerkin-free​​​‌ model is thus proposed,‌ combining CFD for accurately‌​‌ describing the WEC near-field,​​ with POD for efficient​​​‌ far-field wave propagation modeling.‌ The two systems are‌​‌ coupled using a domain​​ decomposition-inspired strategy (Figure 16​​​‌), ensuring bidirectional information‌ exchange for precise flow‌​‌ reconstruction and accurate representation​​ of the floater dynamics.​​​‌ This approach has potential‌ broader applications, serving as‌​‌ an advanced far-field boundary​​ condition in problems involving​​​‌ wave propagation.

Figure 16

Snapshot of‌ the air-water interface. The‌​‌ green domain represents a​​ zoom on the entire​​​‌ simulation domain, the violet‌ domains represent the total‌​‌ support of the coupling​​ technique, given by both​​​‌ the overlapping domain (around‌ the sphere) and a‌​‌ sensor locations for the​​​‌ incoming wave. The ratio​ of the coupling computational​‌ domain to the total​​ simulation domain is 0​​​‌.015%,​ pointing out the significant​‌ CPU savings.

Numerical results​​ on different wave conditions​​​‌ (Figure 17) prove​ the versatility of the​‌ coupling technique, both for​​ in-sample reconstruction (IS, where​​​‌ the POD basis is​ computed with a database​‌ from the baseline condition​​ W0), and​​​‌ an out-of-sample prediction (OOS,​ where the POD basis​‌ is computed with a​​ database from conditions W​​​‌1 and W2​).

Figure 17

Visualization of the​‌ tested waves. The target​​ wave, W0,​​​‌ has characteristics (wave height​ and wave period) equal​‌ to the mean of​​ the characteristics of the​​​‌ other two waves, W​1 and W2​‌, used for the​​ OOS test.

In the​​​‌ OOS case, the L2​ relative errors are slightly​‌ higher than those in​​ the IS case but​​​‌ remain comparable, with all​ errors on the order​‌ of 𝒪(10​​-4).​​​‌ The time evolution of​ the vertical translation of​‌ the floating body and​​ the vertical force acting​​​‌ on it are shown​ in Figure 18.​‌

Figure 18

Evolution of the force​​ acting on the sphere​​​‌ and the heave motion​ over time. The solutions​‌ from the coupled model​​ (hf+POD) are compared to​​​‌ the high-fidelity solution used​ to build the basis​‌ functions (HF).

With only​​ slight dissipation at the​​​‌ peaks and troughs, the​ IS case's temporal evolution​‌ of the force and​​ body position nearly matches​​​‌ the one in the​ reference high-fidelity (HF) solution.​‌ Although the overall behavior​​ is still accurate, there​​​‌ is a slightly larger​ difference between the reference​‌ and the predicted solution​​ in the OOS case.​​​‌ In this case, there​ is an observable phase​‌ shift and a higher​​ degree of dissipation, which​​​‌ may be impacted by​ the time step selected.​‌ The phase shift is​​ likely due to the​​​‌ training dataset containing wave​ periods different from the​‌ target period. In addition​​ to strong CPU savings,​​​‌ the computational time of​ the simulations passes from​‌ approximately 10 hours and​​ 30 minutes on 48​​​‌ processors, to less than​ 4 hours, using only​‌ 6 processors.

9 Bilateral​​ contracts and grants with​​​‌ industry

9.1 Bilateral contracts​ with industry

Participants: Michel​‌ Bergmann, Angelo Iollo​​, Tommaso Taddei.​​​‌

  • Contrat accompagnement Cifre Ingeliance​ (M. Truel) - du​‌ 01/05/2023 au 30/04/2026
  • Contrat​​ accompagnement EDF (A. Moussaddak)​​​‌ - du 01/12/2023 au​ 30/11/2026

10 Partnerships and​‌ cooperations

10.1 International initiatives​​

10.1.1 Associate Teams in​​​‌ the framework of an​ Inria International Lab or​‌ in the framework of​​ an Inria International Program​​​‌

Participants: Michel Bergmann,​ Alessia Del Grosso,​‌ Angelo Iollo, Tommaso​​ Taddei.

ROHM
  • Title:​​​‌
    Reduced Order Hybrid Models​
  • Duration:
    2023 -> 2025​‌
  • Coordinator:
    Charbel Farhat (cfarhat@stanford.edu)​​
  • Partners:
    • Stanford University Stanford​​​‌ (États-Unis)
  • Inria contact:
    Angelo​ Iollo
  • Summary:
    The ROHM​‌ project is devoted to​​ mathematical models that combine​​​‌ partial differential equations and​ prior solutions of such​‌ models in order to​​ reduce the size of​​ the problem. In particular,​​​‌ building on the collaboration‌ previously undertaken in the‌​‌ previous associated MARE team,​​ it is intended to​​​‌ explore two complementary aspects‌ of reduced modeling. On‌​‌ the one hand, it​​ is intended to combine​​​‌ the notion of solution‌ mapping learned in the‌​‌ solution space developed at​​ Bordeaux with the projection​​​‌ space partitioning technique developed‌ at Stanford. On the‌​‌ other hand, it is​​ intended to combine low-fidelity​​​‌ models and high-fidelity models‌ in physical space or‌​‌ time in order to​​ be able to deal​​​‌ with strongly multiscale problems.‌
SPADES
  • Title:
    Structure-Preserving Approximations‌​‌ of Dynamical systems in​​ Engineering and Science
  • Duration:​​​‌
    2024 ->
  • Coordinator:
    Benjamin‌ Sanderse (b.sanderse@cwi.nl)
  • Partners:
    • CWI‌​‌ Amsterdam (the Netherlands)
  • Inria​​ contact:
    Tommaso Taddei and​​​‌ Alessia Del Grosso
  • Summary:‌
    Model order reduction (MOR)‌​‌ of parametric PDEs is​​ a well-established field in​​​‌ scientific computing that aims‌ to reduce the marginal‌​‌ cost associated with the​​ solution to parametric systems:​​​‌ MOR is motivated by‌ many-query (optimization, parameter sweeps)‌​‌ and real-time (interactive design,​​ monitoring) applications, which naturally​​​‌ arise in the field‌ of continuum mechanics. Despite‌​‌ the numerous examples of​​ applications of MOR to​​​‌ large-scale industrial problems, the‌ practical deployment of MOR‌​‌ techniques remains limited in​​ computational fluid dynamics (CFD).​​​‌ To address the current‌ limitations of MOR methods,‌​‌ several authors have proposed​​ structure-preserving projection techniques and​​​‌ nonlinear data compression methods:‌ the former refer to‌​‌ a class of methods​​ that aim to preserve​​​‌ notable properties (e.g., positivity,‌ entropy conservation) of the‌​‌ solution to the underlying​​ PDE, which are not​​​‌ necessarily guaranteed at the‌ reduced-order level; the latter‌​‌ refer to a class​​ of methods that exploit​​​‌ a nonlinear ansatz to‌ estimate the state field.‌​‌ The objective of the​​ Associate Team SPADES between​​​‌ Inria Team MEMPHIS (PI:‌ Tommaso Taddei) and CWI‌​‌ (PI: Benjamin Sanderse) is​​ to devise effective structure-preserving​​​‌ nonlinear model reduction techniques‌ for unsteady nonlinear PDEs‌​‌ that arise in computational​​ fluid dynamics (CFD). The​​​‌ project benefits from the‌ very complementary expertise in‌​‌ nonlinear approximation methods and​​ structure-preserving reduced-order formulations of​​​‌ the two partners, and‌ has the potential to‌​‌ address the grand challenges​​ of model reduction techniques​​​‌ for a broad range‌ of applications in CFD.‌​‌

10.2 National initiatives

  • ANR​​ (national agency for research​​​‌ funding) DRAGON2.
    • Principal‌ investigators: Michel Bergmann
    • Partners:‌​‌ CNRS/Université de Poitiers/Inria. 27​​ k€+ 1 PhD.
    • Summary:​​​‌ The goal is study‌ the aquatic swimming a‌​‌ several snakes using biomimetism​​ and bioinspiration. In this​​​‌ project, we have experimental‌ data for snake swimming,‌​‌ and we are building​​ a numerical twin to​​​‌ compute integral quantities like‌ the efficiency. Reinforcement learning‌​‌ is also considered to​​ optimize the snake swimming.​​​‌
  • ANR (national agency for‌ research funding) RedLum.‌​‌
    • Principal investigators:Tommaso Taddei​​ .
    • Partners: Team ACTA​​​‌ at INRAE Rennes.
    • Summary:‌ REDLUM is a joint‌​‌ project between the team​​ ACTA at INRAE Rennes​​​‌ and the team MEMPHIS‌ at Inria Bordeaux; the‌​‌ project will fund a​​ PhD thesis in October​​​‌ 2024: the selected student‌ will join team MEMPHIS‌​‌ in Bordeaux and will​​​‌ work closely with the​ other partners of the​‌ project. The objective of​​ REDLUM is to develop​​​‌ a model reduction procedure​ for turbulent flows with​‌ unknown boundary conditions; the​​ ultimate goal is to​​​‌ devise a rapid and​ reliable simulation tool to​‌ tackle real-time data assimilation​​ tasks in agricultural sciences.​​​‌ The distinctive methodological feature​ of the approach that​‌ we wish to develop​​ is a stochastic closure​​​‌ model to adequately approximate​ the dynamics of the​‌ low-dimensional coherent structures of​​ the system.
  • Inria Exploratory​​​‌ Action: AM2OR (Adaptive​ meshes for model order​‌ reduction).
    • Principal investigators:​​ Nicolas Barral (Inria team:​​​‌ Cardamom), Tommaso Taddei. 14​ k€+ 1 PhD +​‌ 1 PostDoc.
    • Summary: Mesh​​ adaptation and model order​​​‌ reduction both aim at​ reducing significantly the computational​‌ cost of numerical simulations​​ by taking advantage of​​​‌ the solution's features. Model​ order reduction is a​‌ method that builds lighter​​ surrogate models of a​​​‌ system's response over a​ range of parameters, which​‌ is particularly useful in​​ the solution of design​​​‌ and optimization inverse problems.​ Reduced-order models rely on​‌ a high-fidelity (e.g., finite​​ element) approximation that should​​​‌ be sufficiently accurate over​ the whole range of​‌ parameters considered: in presence​​ of structures such as​​​‌ shocks and boundary layers,​ standard mesh refinement techniques​‌ would lead to high-fidelity​​ models of intractable size.​​​‌ In this project, we​ propose a novel adaptive​‌ procedure to simultaneously construct​​ a high-fidelity mesh (and​​​‌ associated discretisation) and a​ reduced-order model for a​‌ range of parameters, with​​ particular emphasis on inverse​​​‌ problems in computational fluid​ dynamics.

11 Dissemination

11.1​‌ Promoting scientific activities

11.1.1​​ Scientific events: organisation

  • Michel​​​‌ Bergmann , Alessia Del​ Grosso , Angelo Iollo​‌ and Tommaso taddei have​​ organbized the ARIA Workshop​​​‌ 2025 in Birdart, Spetember​ 2025

    link.

Reviewer​‌ - reviewing activities

 

All​​ team members are reviewers​​​‌ for the most infuencial​ journals in our community​‌ (at least one per​​ month for permanent reseachers):​​​‌ Journal of Computional Physics,​ SIAM Journal of SCientific​‌ Computing, Physics of Fluids,​​ ...

11.1.2 Invited talks​​​‌

  • Angelo Iollo : 2025​ décembre. Conférencier invité à​‌ l’Institute for Mathematical &​​ Statistical Innovation, University of​​​‌ Chicago. link
  • Angelo Iollo​ : 2025 novembre. Conférencier​‌ invité au workshop Numerical​​ Approaches for PDEs, ETNA,​​​‌ Catane. link
  • Angelo Iollo​ : 2025 février 22.​‌ Sousse. Conférencier invité à​​ Mathematics, AI and Applications​​​‌ 2025. link
  • Angelo Iollo​ : 2025 février 18-22​‌ Hammamet, Tunisia. Cimpa Research​​ School Control, Optimization and​​​‌ Model Reduction In Machine​ Learning. 6h of short​‌ course on model reduction.​​ link
  • Tommaso Taddei :​​​‌ Invited speaker at the​ workshop on “Scientific Machine​‌ Learning: error control and​​ analysis”, January 2025. Besançon​​​‌ (France), Registration in​ bounded domains for model​‌ reduction of parametric conservation​​ laws.link
  • Tommaso Taddei​​​‌ : Invited speaker at​ the conference Shark-FV, May​‌ 2025. Minho (Portugal)Registration​​ in bounded domains for​​​‌ model reduction of parametric​ conservation laws.link
  • Michel​‌ Bergmann : Invited speaker​​ at the Institut Henri​​​‌ Poincaré for the CEA-SMAI/GAMNI​ Mécanique de Fluides Numériques,​‌ January 2025. Paris (France)​​, From Linear to​​ Nonlinear Interpolation: Reduced Basis​​​‌ and Optimal Transport for‌ Data Recycling in Incompressible‌​‌ Flow Simulations. link
  • Michel​​ Bergmann : Invited speaker​​​‌ at the Conférence Climath‌ : Coastal flows, extreme‌​‌ waves and wave-structure interaction,​​ November 2025. Bordeaux (France)​​​‌, From CFD approach‌ to wave-structure interactions. link‌​‌
  • Alessia Del Grosso :​​ Invited speaker at the​​​‌ workshop ETNA November 2025.‌ Catania (Italy), A‌​‌ non-conservative scheme for hyperelastic​​ materials circumventing the involution​​​‌ constraint link
  • Alessia Del‌ Grosso : Invited speaker‌​‌ at the workshop HyPNuT​​ November 2025. Amiens (France)​​​‌, A non-conservative scheme‌ for hyperelastic materials circumventing‌​‌ the involution constraint link​​
  • Alessia Del Grosso :​​​‌ Invited speaker at the‌ workshop ARIA 2025. September‌​‌ 2025. Bidart (France),​​ Collocation-based ROMs: analysis and​​​‌ applications link
  • Alessia Del‌ Grosso : Invited speaker‌​‌ at the workshop 3C:​​ Challenges in Computational methods​​​‌ for Complex environmental applications.‌ May 2025. Le Bourget-du-Lac‌​‌ (France), From supersonic​​ to low Mach number​​​‌ flows using cell-centered finite‌ volume multi-point schemes link‌​‌

11.1.3 Leadership within the​​ scientific community

  • Michel Bergmann​​​‌ is Délégué Scientifique Adjoint‌ (DSA) of the centre‌​‌ Inria de l'université de​​ Bordeaux (since July 2024).​​​‌ He is a member‌ of inria evaluation committee,‌​‌ the scientific committee of​​ the institute of mathematics​​​‌ in Bordeaux (IMB), is‌ member of the scientific‌​‌ committee of méso-centre aquitain​​ MCIA, and is member​​​‌ of the CDT (commission‌ de développements technologiques) at‌​‌ Inria.
  • Angelo Iollo is​​ PI with Denis Sipp​​​‌ of Onera of the‌ Chair PROVE, endowed by‌​‌ a grant of Region​​ Nouvelle Aquitaine and Onera.​​​‌ The chair is endowed‌ with PhD grants, PostDocs‌​‌ and funding for research​​ animation. He is also​​​‌ the PI of the‌ newly created common team‌​‌ Inria-ONERA MONHADE (since 1st​​ Novemebre 2025).

11.1.4 Scientific​​​‌ expertise

Angelo Iollo was‌ expert for the IdEX‌​‌ initiative of the University​​ of Nice as well​​​‌ as expert for the‌ University of Modena program‌​‌ FAR.

11.2 Teaching -​​ Supervision - Juries -​​​‌ Educational and pedagogical outreach‌

Two members of the‌​‌ team are Professor (Angelo​​ Iollo) or Assistant Professor​​​‌ (Afaf Bouharguane) at Université‌ de Bordeaux and have‌​‌ teaching duties, which consist​​ in courses and practical​​​‌ exercises in numerical analysis‌ and scientific computing. Michel‌​‌ Bergmann (DR) teaches around​​ 64 hours per year​​​‌ (courses on renewable energies‌ and practical exercises in‌​‌ programming for scientific computing).​​ Tommaso Taddei (CR) teaches​​​‌ around 50 hours per‌ year (practical exercises in‌​‌ numerical analysis and scientific​​ computing). Alessia Del Grosso​​​‌ (ISFP) teaches around 30‌ hours per year (mathematics‌​‌ for engineering).

11.2.1 Supervision​​

Michel Bergmann supervises or​​​‌ co-supervises the PhD theses‌ of Maxime Chapron, Mathias‌​‌ Truel and Karl Maroun.​​

Angelo Iollo supervises or​​​‌ co-supervises the PhD theses‌ of Jon Labatut, Elise‌​‌ Declerk, Mathias Truel, Marc-Oliveir​​ Potin and Alexis Valls.​​​‌

Tommaso Taddei supervises or‌ co-supervises the PhD theses‌​‌ of Jon Labatut, Abdessamad​​ Moussaddak, Ishak Tifouti and​​​‌ Alexis Valls.

Alessia Del‌ Grosso co-supervises the PhD‌​‌ theses of Lucas Brelivet​​ and Giorgio Musso.

11.2.2​​​‌ Juries

Michel Bergmann was‌ the president of the‌​‌ jury for the PhD​​​‌ of Lou Guérin (Poitiers​ University); he further reviewed​‌ the PhD thesis of​​ Clément Caron (University of​​​‌ Ile de la Réunion)​ and Céline Van Landeghem​‌ (Strasbourg University). He was​​ the President of Inria​​​‌ selection board (jury d'admissibilité)​ for the recruitment of​‌ CRCN (junior researchers) and​​ ISFP at the Centre​​​‌ Inria de l'université de​ Rennes, and member of​‌ the selection board (jury​​ d'admissibilité) for the recruitment​​​‌ of DR2 (research Director,​ Senior Researchers).

Angelo Iollo​‌ was reviewer of the​​ PhD thesis of Raphael​​​‌ Villiers, Université de Poitiers;​ reviewer of the PhD​‌ thesis of Moaad Khamlich,​​ SISSA; reviewer of the​​​‌ HDR of Lionel Mathelin,​ Cnrs; reviewer of the​‌ PhD theis of Erica​​ Tamellini, Politecnico di Milano.​​​‌

11.2.3 Specific official responsibilities​ in science outreach structures​‌

Michel Bergmann leads the​​ storytelling efforts for the​​​‌ Energy research axis at​ Centre Inria de l'université​‌ de Bordeaux.

Tommaso Taddei​​ was a member of​​​‌ the CUMI-R committee and​ of the CDT before​‌ july. Since July, Alessia​​ Del Grosso is a​​​‌ member of the CUMI-R​ committee and of the​‌ CDT.

11.2.4 Productions (articles,​​ videos, podcasts, serious games,​​​‌ ...)

Michel Bergmann and​ Angelo Iollo have participed​‌ to a presentation article​​ on the new Inria-Onera​​​‌ common team MONHADE link​.

Michel Bergmann :​‌ video "une minute avec"​​ link

Alessia Del Grosso​​​‌ : video "une minute​ avec" link

12 Scientific​‌ production

12.1 Major publications​​

  • 1 articleE.E.​​​‌ Abbate, A.A.​ Iollo and G.G.​‌ Puppo. An all-speed​​ relaxation scheme for gases​​​‌ and compressible materials.​Journal of Computational Physics​‌3512017, 1-24​​HALDOI
  • 2 article​​​‌N.Nicolas Barral,​ T.Tommaso Taddei and​‌ I.Ishak Tifouti.​​ Registration-based model reduction of​​​‌ parameterized PDEs with spatio-parameter​ adaptivity.Journal of​‌ Computational Physics499February​​ 2024, 112727HAL​​​‌DOIback to text​
  • 3 articleL.Luis​‌ Benetti Ramos, O.​​Olivier Marquet, M.​​​‌Michel Bergmann and A.​Angelo Iollo. Fluid--solid​‌ Floquet stability analysis of​​ self-propelled heaving foils.​​​‌Journal of Fluid Mechanics​9102021, A28​‌HALDOI
  • 4 article​​M.M. Bergmann,​​​‌ C.-H.Charles-Henri Bruneau and​ A.A. Iollo.​‌ Enablers for robust POD​​ models.Journal of​​​‌ Computational Physics2282​2009, 516--538
  • 5​‌ articleM.M. Bergmann​​, J.J. Hovnanian​​​‌ and A.A. Iollo​. An accurate cartesian​‌ method for incompressible flows​​ with moving boundaries.​​​‌Communications in Computational Physics​1552014,​‌ 1266--1290back to text​​
  • 6 articleM.M.​​​‌ Bergmann and A.A.​ Iollo. Bioinspired swimming​‌ simulations.Journal of​​ Computational Physics3232016​​​‌, 310 - 321​
  • 7 articleM.M.​‌ Bergmann and A.A.​​ Iollo. Modeling and​​​‌ simulation of fish-like swimming​.Journal of Computational​‌ Physics23022011​​, 329 - 348​​​‌
  • 8 articleM.Michel​ Bergmann. Numerical modeling​‌ of a self propelled​​ dolphin jump out of​​​‌ water.Bioinspiration and​ Biomimetics1762022​‌, 065010HALDOI​​back to text
  • 9​​ articleF.F. Bernard​​​‌, A.A. Iollo‌ and G.G. Puppo‌​‌. Accurate Asymptotic Preserving​​ Boundary Conditions for Kinetic​​​‌ Equations on Cartesian Grids‌.Journal of Scientific‌​‌ Computing2015, 34​​
  • 10 articleA.A.​​​‌ Bouharguane, A.A.‌ Iollo and L.L.‌​‌ Weynans. Numerical solution​​ of the Monge--Kantorovich problem​​​‌ by density lift-up continuation‌.ESAIM: Mathematical Modelling‌​‌ and Numerical Analysis49​​61577November 2015​​​‌
  • 11 inproceedingsM.Maxime‌ Chapron, C.Christophe‌​‌ Blondeau, I.Itham​​ Salah El Din,​​​‌ D.Denis Sipp and‌ M.Michel Bergmann.‌​‌ Clustered Active Subspaces Applied​​ to Aerodynamic Shape Optimisation​​​‌.9th European Congress‌ on Computational Methods in‌​‌ Applied Sciences and Engineering​​ECCOMAS 2024 - 9th​​​‌ European Congress on Computational‌ Methods in Applied Sciences‌​‌ and EngineeringLisbonne, Portugal​​October 2024HALback​​​‌ to text
  • 12 inproceedings‌M.Maxime Chapron,‌​‌ C.Christophe Blondeau,​​ I.Itham Salah El​​​‌ Din, D.Denis‌ Sipp and M.Michel‌​‌ Bergmann. Clustered Active​​ Subspaces for Aerodynamic Shape​​​‌ Optimization.AIAA SCITECH‌ 2025 ForumAIAA SCITECH‌​‌ 2025 ForumOrlando, United​​ StatesAmerican Institute of​​​‌ Aeronautics and AstronauticsJanuary‌ 2025, AIAA 2025-0652‌​‌HALDOIback to​​ text
  • 13 articleA.​​​‌A. De Brauer,‌ A.A. Iollo and‌​‌ T.T. Milcent.​​ A Cartesian Scheme for​​​‌ Compressible Multimaterial Models in‌ 3D.Journal of‌​‌ Computational Physics3132016​​, 121-143back to​​​‌ text
  • 14 articleA.‌Angelo Iollo and T.‌​‌Tommaso Taddei. Mapping​​ of coherent structures in​​​‌ parameterized flows by learning‌ optimal transportation with Gaussian‌​‌ models.Journal of​​ Computational Physics471111671​​​‌2022, 111671HAL‌DOIback to text‌​‌
  • 15 articleA.Angelo​​ Iollo and T.Tommaso​​​‌ Taddei. Point-set registration‌ in bounded domains via‌​‌ the Fokker–Planck equation.​​Comptes Rendus. Mathématique363​​​‌G82025, 809-824‌HALDOIback to‌​‌ text
  • 16 articleF.​​F. Luddens, M.​​​‌M. Bergmann and L.‌L. Weynans. Enablers‌​‌ for high-order level set​​ methods in fluid mechanics​​​‌.International Journal for‌ Numerical Methods in Fluids‌​‌79December 2015,​​ 654-675
  • 17 articleK.​​​‌Karl Maroun, P.‌Philippe Traoré and M.‌​‌Michel Bergmann. Data-driven​​ optimal control of undulatory​​​‌ swimming.Physics of‌ Fluids367September‌​‌ 2024HALDOIback​​ to text
  • 18 article​​​‌T.T. Meuel,‌ Y. L.Y. L.‌​‌ Xiong, P.P.​​ Fischer, C.-H.Charles-Henri​​​‌ Bruneau, M.M.‌ Bessafi and H.H.‌​‌ Kellay. Intensity of​​ vortices: from soap bubbles​​​‌ to hurricanes.Scientific‌ Reports3December 2013‌​‌, 3455 (1-7)
  • 19​​ articleG.Guillaume Ravel​​​‌, M.Michel Bergmann‌, A.Alain Trubuil‌​‌, J.Julien Deschamps​​, R.Romain Briandet​​​‌ and S.Simon Labarthe‌. Inferring characteristics of‌​‌ bacterial swimming in biofilm​​ matrix from time-lapse confocal​​​‌ laser scanning microscopy.‌eLife11June 2022‌​‌HALDOIback to​​ text
  • 20 articleM.​​​‌Michele Romanelli, S.‌Samir Beneddine, I.‌​‌Ivan Mary, H.​​​‌Heloise Beaugendre, M.​Michel Bergmann and D.​‌Denis Sipp. Data-driven​​ wall models for Reynolds​​​‌ Averaged Navier-Stokes simulations.​International Journal of Heat​‌ and Fluid Flow99​​January 2023, 109097​​​‌HALDOIback to​ textback to text​‌
  • 21 articleM.Michele​​ Romanelli, S.Samir​​​‌ Beneddine, I.Ivan​ Mary, H.Héloïse​‌ Beaugendre, M.Michel​​ Bergmann and D.Denis​​​‌ Sipp. Efficient and​ accurate data-driven wall modelling​‌ strategy for Reynolds averaged​​ Navier–Stokes simulations.Journal​​​‌ of Computational Physics538​October 2025, 114128​‌HALDOIback to​​ textback to text​​​‌
  • 22 thesisM.Michele​ Romanelli. Deep Wall​‌ Models for Aerodynamic Simulations​​.Université de Bordeaux​​​‌December 2024HALback​ to text
  • 23 thesis​‌T.Tommaso Taddei.​​ Some contributions to model​​​‌ reduction of parametric systems​ in nonlinear mechanics.​‌École doctorale Mathématiques et​​ Informatique, Université de Bordeaux​​​‌April 2024HALback​ to text
  • 24 thesis​‌I.Ishak Tifouti.​​ Construction of reduced-order models​​​‌ with mesh adaptation.​Université de BordeauxNovember​‌ 2025HALback to​​ text
  • 25 articleY.​​​‌ L.Y. L. Xiong​, C.-H.Charles-Henri Bruneau​‌ and H.H. Kellay​​. A numerical study​​​‌ of two dimensional flows​ past a bluff body​‌ for dilute polymer solutions​​.Journal of Non-Newtonian​​​‌ Fluid Mechanics1962013​, 8-26

12.2 Publications​‌ of the year

International​​ journals

Invited conferences​​​‌

International peer-reviewed conferences‌​‌

Conferences‌​‌ without proceedings

Doctoral dissertations and habilitation​​ theses

  • 43 thesisA.​​​‌Alexis Tardieu. ADER-DG​ approaches for the nonlinear​‌ advection-diffusion : application to​​ the incompressible Navier-Stokes equations​​​‌.Université de Bordeaux​November 2025HALback​‌ to text

Reports &​​ preprints

12.3 Cited​‌ publications

  • 48 articleP.​​P. Angot, C.-H.​​​‌Charles-Henri Bruneau and P.​P. Fabrie. A​‌ penalization method to take​​ into account obstacles in​​​‌ a incompressible flow.​Numerische Mathematik814​‌1999, 497-520back​​ to text
  • 49 article​​​‌S.Stavros Avgerinos,​ F.Florian Bernard,​‌ A.Angelo Iollo and​​ G.Giovanni Russo.​​​‌ Linearly implicit all Mach​ number shock capturing schemes​‌ for the Euler equations​​.Journal of Computational​​​‌ Physics3932019,​ 278-312URL: https://www.sciencedirect.com/science/article/pii/S0021999119302530DOI​‌back to text
  • 50​​ articleJ.Joshua Barnett​​​‌ and C.Charbel Farhat​. Quadratic approximation manifold​‌ for mitigating the Kolmogorov​​ barrier in nonlinear projection-based​​​‌ model order reduction.​J. Comput. Phys.464​‌2022, 111348back​​ to text
  • 51 article​​P.P.T. Barton,​​​‌ D.D. Drikakis,‌ E.E. Romenski and‌​‌ V.V.A. Titarev.​​ Exact and approximate solutions​​​‌ of Riemann problems in‌ non-linear elasticity.Journal‌​‌ of Computational Physics228​​182009, 7046-7068​​​‌back to text
  • 52‌ articleS.Stefano Bianchini‌​‌. Hyperbolic limit of​​ the Jin‐Xin relaxation model​​​‌.Communications on Pure‌ and Applied Mathematics59‌​‌05 2006, 688​​ - 753DOIback​​​‌ to text
  • 53 article‌A. D.A. De‌​‌ Brauer, A.A.​​ Iollo and T.T.​​​‌ Milcent. A Cartesian‌ scheme for compressible multimaterial‌​‌ models in 3D.​​Journal of Computational Physics​​​‌3132016, 121-143‌URL: http://www.sciencedirect.com/science/article/pii/S0021999116000966DOIback‌​‌ to text
  • 54 article​​B.B Cantwell and​​​‌ D.D Coles.‌ An experimental study of‌​‌ entrainment and transport in​​ the turbulent near wake​​​‌ of a circular cylinder‌.Journal of fluid‌​‌ mechanics1361983,​​ 321--374back to text​​​‌
  • 55 articleS.S.L.‌ Gavrilyuk, N.N.‌​‌ Favrie and R.R.​​ Saurel. Modelling wave​​​‌ dynamics of compressible elastic‌ materials.Journal of‌​‌ Computational Physics2275​​2008, 2941-2969back​​​‌ to text
  • 56 book‌S.S.K. Godunov.‌​‌ Elements of continuum mechanics​​.Nauka Moscow1978​​​‌back to text
  • 57‌ articleA. D.A.‌​‌ Del Grosso, M.​​ C.M. Castro Díaz​​​‌, C.C. Chalons‌ and T. M.T.‌​‌ Morales de Luna.​​ On well-balanced implicit-explicit Lagrange-projection​​​‌ schemes for two-layer shallow‌ water equations.Applied‌​‌ Mathematics and Computation442​​2023, 127702URL:​​​‌ https://www.sciencedirect.com/science/article/pii/S0096300322007706DOIback to‌ text
  • 58 phdthesisX.‌​‌X Jin. Construction​​ d'une chaîne d'outils numériques​​​‌ pour la conception aérodynamique‌ de pales d'éoliennes.‌​‌Université de Bordeaux2014​​back to text
  • 59​​​‌ articleP. D.P.‌ D. Lax and R.‌​‌ D.R. D. Richtmyer​​. Survey of the​​​‌ stability of linear finite‌ difference equations.Communications‌​‌ on Pure and Applied​​ Mathematics921956​​​‌, 267-293URL: https://onlinelibrary.wiley.com/doi/abs/10.1002/cpa.3160090206‌DOIback to text‌​‌
  • 60 articleG.G.H.​​ Miller and P.P.​​​‌ Colella. A Conservative‌ Three-Dimensional Eulerian Method for‌​‌ Coupled Solid-Fluid Shock Capturing​​.Journal of Computational​​​‌ Physics18312002‌, 26-82back to‌​‌ text
  • 61 inproceedingsC.​​C. Parés. Path-Conservative​​​‌ Numerical Schemes for Nonconservative‌ Hyperbolic Systems.Hyperbolic‌​‌ Problems: Theory, Numerics, Applications​​Berlin, HeidelbergSpringer Berlin​​​‌ Heidelberg2008, 817--824‌back to text
  • 62‌​‌ bookJ. A.J.​​ A. Sethian. Level​​​‌ Set Methods and Fast‌ Marching Methods.Cambridge‌​‌ University Press, Cambridge, UK​​1999back to text​​​‌
  • 63 articleT.Tommaso‌ Taddei, X.Xuejun‌​‌ Xu and L.Lei​​ Zhang. A non-overlapping​​​‌ optimization-based domain decomposition approach‌ to component-based model reduction‌​‌ of incompressible flows.​​Journal of Computational Physics​​​‌5092024, 113038‌back to text
  • 64‌​‌ articleT.Tommaso Taddei​​, X.Xuejun Xu​​​‌ and L.Lei Zhang‌. High-order implicit Runge-Kutta‌​‌ time integrators for component-based​​ model reduction of FSI​​​‌ problems.arXiv preprint‌ arXiv:2512.233632025back to‌​‌ textback to text​​​‌
  • 65 articleT.Tommaso​ Taddei, X.Xuejun​‌ Xu and L.Lei​​ Zhang. Optimization-based model​​​‌ order reduction of fluid-structure​ interaction problems.Journal​‌ of Computational Physics2025​​, 114084back to​​​‌ text
  • 66 articleA.​Andrea Thomann. Semi-implicit​‌ relaxed finite volume schemes​​ for hyperbolic multi-scale systems​​​‌ of conservation laws.​Journal of Computational Physics​‌5392025, 114263​​URL: https://www.sciencedirect.com/science/article/pii/S0021999125005467DOIback​​​‌ to text
  • 67 incollection​S.Stefan Turek and​‌ J.Jaroslav Hron.​​ Proposal for numerical benchmarking​​​‌ of fluid-structure interaction between​ an elastic object and​‌ laminar incompressible flow.​​Fluid-structure interaction: modelling, simulation,​​​‌ optimisationSpringer2006,​ 371--385back to text​‌