The Onera elsA CFD software: input from research and feedback from industry

L Cambier, S Heib, S Plot - Mechanics & Industry, 2013 - cambridge.org
The Onera elsA CFD software is both a software package capitalizing the innovative results
of research over time and a multi-purpose tool for applied CFD and multi-physics. The …

Dissipation and time step scaling strategies for low and high Mach number flows

S Seraj, A Yildirim, JL Anibal, JRRA Martins - Journal of Computational …, 2023 - Elsevier
Aircraft aerodynamic design often involves evaluating flow conditions that span low
subsonic to transonic or even supersonic Mach numbers. Compressible flow solvers are a …

An implicit splitting scheme with characteristic boundary conditions for compressible reactive flows on unstructured grids

M Pries, A Fiolitakis, P Gerlinger - Journal of Computational and Applied …, 2024 - Elsevier
The computation of combustion instabilities requires efficient numerical solvers. For low
Mach number compressible flows splitting schemes provide an adequate family of solution …

Simulation and adjoint-based design for variable density incompressible flows with heat transfer

TD Economon - AIAA Journal, 2020 - arc.aiaa.org
This paper details the development and implementation of a density-based solution
approach for simulation and design in variable density incompressible flows with heat …

The more actual macroscopic equations recovered from lattice Boltzmann equation and their applications

J Lu, H Lei, C Shu, C Dai - Journal of Computational Physics, 2020 - Elsevier
Chapman-Enskog (CE) expansion analysis shows that the lattice Boltzmann equation (LBE)
can recover the second-order continuity and NS equations of the weakly compressible …

[PDF][PDF] Aeropropulsive performance analysis of the NOVA configurations

L Wiart, O Atinault, JC Boniface, R Barrier - 30th Congress of the …, 2016 - icas.org
In order to evaluate the potential of UHBR (Ultra High Bypass Ratio) turbofan engines for the
replacement of existing medium-haul aircraft, four different NOVA (Nextgen Onera Versatile …

Low-speed preconditioning for strongly coupled integration of Reynolds-averaged Navier–Stokes equations and two-equation turbulence models

MS Campobasso, M Yan, A Bonfiglioli… - Aerospace Science and …, 2018 - Elsevier
Computational fluid dynamics codes using the density-based compressible flow formulation
of the Navier–Stokes equations have proven to be very successful for the analysis of high …

Preconditioned boundary-implicit subiterative DDADI method for accuracy and efficiency enhancement in low-Mach number flows

F Liao, Y Jin - Computers & Fluids, 2023 - Elsevier
For low-speed turbulent flows governed by compressible Navier–Stokes equations, the
large disparity of phase velocities between hydrodynamic wave and acoustic wave leads to …

[PDF][PDF] Improving the Performance of a Compressible RANS Solver for Low and High Mach Number Flows

S Seraj, A Yildirim, JL Anibal… - … on Computational Fluid …, 2022 - researchgate.net
The aerodynamic design of aircraft often involves evaluating flow conditions that span low
subsonic to transonic, or even supersonic Mach numbers. Compressible flow solvers are a …

[PDF][PDF] Prévision de la transition laminaire-turbulent dans filecode elsA par la méthode des paraboles

G Bégou - 2018 - researchgate.net
Une composante importante de la conception des ailes d'avion est l'évaluation de leurs
performances, notamment en termes de trainée. En régime subsonique, celle-ci est due en …