Prediction of fluctuating pressure loads produced by shock-induced turbulent boundary layer separation-Reference-Cited by-同舟云学术

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Prediction of fluctuating pressure loads produced by shock-induced turbulent boundary layer separation

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:Fluid Dynamics Conference
language:
Short-container-title:

Author:

Barter J.¹,Dolling David¹

Affiliation:

1. Texas, Univ., Austin

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2043

Reference15 articles.

1. Chapman, D. R.,D. M. Kuehn, and H. K. Larson, "InvestigationofSeparatedFlowsin Supersonicand Subsonic Streamswith Emphasisonthe Effect of Transition," NACA Report 1356,1958.

2. Pozefsky, P., R.D. Blevins,and A.L. Laganelli, "Thermo-Vibro-Acoustic Loadsand Fatigueof Hypersonic Flight VehicleStructures," AFWALTR-89-3014, Feb.1989.

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