Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations-Reference-Cited by-同舟云学术

Development and application of Spalart–Allmaras one equation turbulence model to three-dimensional supersonic complex configurations

Published:2002-03 Issue:3 Volume:6 Page:171-183
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Deck Sébastien,Duveau Philippe,d'Espiney Paulo,Guillen Philippe

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Filtering algebraic turbulence models for supersonic high-incidence missile flows;Amato,1998

2. Introduction to Turbulence Modeling for Compressible Flows;Aupoix,2000

3. B. Baldwin, T.J. Barth, A one-equation turbulence transport model for high Reynolds number wall-bounded flows, AIAA Paper 91-0610, 1991

4. B.S. Baldwin, H. Lomax, Thin layer approximation of algebraic model for separated flows, AIAA Paper 78-0257, 1978

5. S. Ben Khelil, Simulation numérique d'écoulements turbulents autourde configurations complexes. Application au roulis induit des missiles, PhD thesis, Université de Paris 13, 1998

Cited by 117 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Resolvent Analysis of Subsonic Jets: Resonance Mechanisms and Wave Reflections;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

2. Numerical study of shock wave boundary layer interaction flows using a novel turbulence model;Physics of Fluids;2024-05-01

3. Numerical Analysis of Turbulent Flow around an Irregularly Shaped Airfoil;2024-03-25

4. Numerical Investigation of a Vortex Diverter Designed for Improving the Performance of the Submerged Inlet;Aerospace;2023-12-30

5. COMPUTATIONAL INVESTIGATION INTO THE EFFECT OF PITCH RATIOS ON B-SERIES PROPELLER PERFORMANCE;J NAV ARCHIT MAR ENG;2023