Lessons Learned from the 2010 AIAA Shock Boundary Layer Interaction Prediction Workshop-Reference-Cited by-同舟云学术

Lessons Learned from the 2010 AIAA Shock Boundary Layer Interaction Prediction Workshop

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Benek John¹

Affiliation:

1. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4825

Reference5 articles.

1. Anderson,B.H.,Tinapple,J.,Surber,L."OptimalControlofShockWaveTurbulentBoundaryLayerInteractions UsingMicroArrayActuation,"AIAAPaperNo.2006-3197,June2006.

2. Unsteadyeffectsinshockwaveinducedseparation.Eds,P.Doerffer,C.Hirsch,J-PDussage,H.Babinsky,andG. Barakos,Springer2010,ISBN978-3-642-03003-1.

3. Compressible Boundary-Layer Predictions at High Reynolds Number Using Hybrid LES/RANS Methods

4. Georgiadis,N.J.,Rizzetta,D.P.,andFureby,C."Large-EddySimulation:CurrentCapabilities,Recommended Practices,andFutureResearch,"AIAAPaperNo.2009-948,January2009.

5. Park,M.A.andCarlson,J.R."TurbulentOutput-BasedAnisotropicAdaptation",AIAAPaperNo.2010-168, January2010.

Cited by 21 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. Structural uncertainty quantification of Reynolds-Averaged Navier–Stokes closures for various shock-wave/boundary layer interaction flows;Chinese Journal of Aeronautics;2023-10

2. Oblique Shock Control with Steady Flexible Panels;AIAA Journal;2020-05

3. Visualization of Separated Flow Features Induced by Cylindrical Protuberance at Hypersonic Speed by Double-Color Oil Flow;Lecture Notes in Electrical Engineering;2019

4. Experimental Study of Turbulent Separated Flowfield Induced by a Perpendicular Blunt Fin;Lecture Notes in Electrical Engineering;2019

5. Numerical Simulations of a Cylinder-Induced Shock Wave/Boundary Layer Interaction;55th AIAA Aerospace Sciences Meeting;2017-01-05