Etude, mise au point et validation de modèles de turbulence compressible. (Development, validation and assessment of turbulence models for compressible flows)

Yohann Perrot · ANZ Journal of Surgery · 2006

Summary

Cette these etudie essentiellement des phenomenes touchant aux domaines aeronautique and spatial traite par simulations numeriques des ecoulement dans les tuyeres de moteur-fusee, les ecoulements d'arriere-corps d'avions, et les Ecoulements supersoniques en presence d'interactions onde de choc/couche limite.

Type: dissertation
Published: 2006-12-19
Cited by: 6
References: 77
Access: Open access
DOI: https://doi.org/10.1111/ans.13190
OpenAlex: https://openalex.org/W26011539
Semantic Scholar: https://api.semanticscholar.org/CorpusID:46149941

Keywords

Humanities, Physics, Philosophy

References

Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approachPhilippe R. Spalart — 1997
Joint European Effort Towards Advanced Rocket Thrust Chamber TechnologyManuel Frey, Axel Preuß, Stève Girard — 2005
Simulation des grandes Echelles d'ecoulements Turbulents Supersoniques. (Large Eddy Simulation of supersonic turbulent flows)Samuel Dubos — 2005
Modélisation et étude numérique de la turbulence compressible en écoulements supersoniquesGuy Douay — 1994
Etude numérique du décollement en tuyères supersoniquesCyril Pilinski — 2002
Turbulence d'une interaction onde de choc/couche limite sur une paroi plane adiabatique ou chaufféeHenri Laurent — 1996
Subgrid-Scale Stress Modelling Based on the Square of the Velocity Gradient TensorFranck Nicoud, F. Ducros — 1999
Second order closure for the calculation of compressible wall bounded flows with an implicit Navier-Stokes solverD. Vandromme, H. Ha Minh, J. R. Viegas — 1984
Flow Processes in Rocket Engine Nozzles with Focus on Flow Separation and Side-LoadsJan Östlund — 2002
Characteristics of turbulence in a boundary layer with zero pressure gradientPhilip S. Klebanoff — 1955
Behandlung von Strömungsproblemen in Raketendüsen bei ÜberexpansionManuel Frey — 2001
The minimal flow unit in near-wall turbulenceJavier Jiménez, Parviz Moin — 1991
Large Eddy simulation of high-Reynolds-number free and wall-bounded flowsChrister Fureby, Fernando F. Grinstein — 2000
Status of Low Separation Prediction in Rocket Nozzles.Manuel Frey, G. Hagemann — 1998
Recent Progress on MILES for High Reynolds Number FlowsFernando F. Grinstein, Christer Fureby — 2002
The numerical computation of turbulent flowsB. E. Launder, D. B. Spalding — 1990
Investigation of Supersonic Flow Separation in NozzlesR. P. Fraser, P. Eisenklam, David Wilkie — 1959
The compressible turbulent shear layer: an experimental studyDimitri Papamoschou, A. Roshko — 1988
Sea level side loads in high-area-ratio rocket enginesL. NAVE, G. COFFEY — 1973
An Analysis of Numerical Errors in Large-Eddy Simulations of TurbulenceSandip Ghosal — 1996

Cited by

Influence of downstream unsteadiness on shock pattern in separated nozzle flowsAlexandre Georges-Picot, A. Hadjadj, J. Herpe — 2014
Simulation numérique de l’écoulement compressible supersonique Application aux tuyères propulsives à combustible liquide hydrogèneEl-Ahcene Mahfoudi, Abderrahmane Gahmousse, Athmane Harizi — 2015
Etude numérique de l’écoulement compressible turbulent dans une tuyère supersoniqueEl-Ahcene Mahfoudi, Abderrahmane Gahmousse, Kamel Talbi — 2023
Design and Numerical Analysis of E-D Nozzle with Throat Radius Investigation in Supersonic Flows: A Comparison Study with Tic NozzleHaif, Sidali, Kbab, Hakim, Benkhedda, Amina — 2024
COMPRESSIBLE FLOW THROUGH A SUPERSONIC NOZZLE-A COMPUTATIONAL APPROACH2016
NUMERICAL STUDY OF THE COMPRESSIBLE FLOW INSIDE A SUPERSONIC NOZZLE TO 2DS. Sellami, O. Kholai — 2015

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