Hypersonic Wind-Tunnel Measurements of Boundary-Layer Pressure Fluctuations-Reference-Cited by-同舟云学术

Hypersonic Wind-Tunnel Measurements of Boundary-Layer Pressure Fluctuations

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:39th AIAA Fluid Dynamics Conference
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Author:

Casper Katya¹,Beresh Steven²,Henfling John²,Spillers Russell²,Pruett Brian²,Schneider Steven¹

Affiliation:

1. Purdue University

2. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4054

Reference43 articles.

1. PREDICTION OF BOUNDARY LAYER PRESSURE FLUCTUATIONS

2. Experimental Determination of the Aeroacoustic Environment about a Slender Cone

3. 4Chaump, L., Martellucci, A., and Monfort, A. “Aeroacoustic Loads Associated with High Beta Re-entry Vehicles,” Tech. Rep. TR-72-138, AFFDL, May 1973, VolumeI.

4. 5Raman, K. “Surface Pressure Fluctuations in Hypersonic Turbulent Boundary Layers,” AIAA Paper 73-997, October

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