Large Eddy Simulation of Shock/Boundary-Layer Interaction-Reference-Cited by-同舟云学术

Large Eddy Simulation of Shock/Boundary-Layer Interaction

Published:2002-10 Issue:10 Volume:40 Page:1935-1944
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Garnier Eric¹,Sagaut Pierre¹,Deville Michel²

Affiliation:

1. ONERA, 92322 Chatillon, France

2. Ecole Polytechnique Federale de Lausanne, CH-1015 Lausanne, Switzerland

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.1552

Reference10 articles.

1. Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary Layers

2. Smits, A. J., and Dussauge, J. P., Turbulent Shear Layers in Supersonic Flow, AIP Press, Woodbury, NY, 1996, pp.285-319.

3. Supersonic and hypersonic shock/boundary-layer interaction database

4. David, E. “Modlisation des coulements Compressibles et Hypersoniques,” Ph.D. Dissertation,Dept. of Engineering, Grenoble Univ., Grenoble, France,June 1993.

Cited by 140 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. Design and aerodynamic characteristics of variable-geometry hypersonic inlet based on shock wave elimination;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-06-23

2. Shock Train Structure in Axisymmetric Domains;AIAA SCITECH 2024 Forum;2024-01-04

3. Large eddy simulations of supersonic flow over a cylinder using an immersed boundary method;AIAA SCITECH 2024 Forum;2024-01-04

4. A high-order fluid–structure interaction framework with application to shock-wave/turbulent boundary-layer interaction over an elastic panel;Journal of Fluids and Structures;2023-08

5. Simulation of the shock wave boundary layer interaction in flat channel with jet injection;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;2023-01-15