Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone-Reference-Cited by-同舟云学术

Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone

Published:2016-04 Issue:4 Volume:54 Page:1250-1263
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Casper Katya M.¹,Beresh Steven J.¹,Henfling John F.¹,Spillers Russell W.¹,Pruett Brian O. M.¹,Schneider Steven P.²

Affiliation:

1. Sandia National Laboratories, Albuquerque, New Mexico 87185

2. Purdue University, West Lafayette, Indiana 47907-1282

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J054033

Reference44 articles.

1. PateS. R.BrownM. D. “Acoustic Measurements in Supersonic Transitional Boundary Layers,” AEDC-TR-69-182, Oct. 1969.

2. JohnsonR. I.MacourekM. N.SaundersH. “Boundary Layer Acoustic Measurements in Transitional and Turbulent Flow at M∞=4.0,” AIAA Paper 1969-344, April 1969.

3. An Experiment to Determine Nose Tip Transition with Fluctuating Pressure Measurements

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

5. PateS. R. “Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic/Hypersonic Wind Tunnels,” AEDC-TR-77-107, March 1978.

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