Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels-Reference-Cited by-同舟云学术

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Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels

Published:2018-01-07 Issue: Volume: Page:
ISSN:
Container-title:2018 AIAA Aerospace Sciences Meeting
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Author:

Duan Lian¹,Choudhari Meelan M.²,Chou Amanda²,Munoz Federico³,Ali S.R.C.³,Radespiel Rolf³,Schilden Thomas⁴,Schroeder Wolfgang⁴,Marineau Eric C.⁵,Casper Katya M.⁶,Chaudhry Ross S.⁷,Candler Graham V.⁷,Gray Kathryn A.⁸,Sweeney Cameron J.⁸,Schneider Steven P.⁸

Affiliation:

1. Missouri University of Science and Technology

2. NASA Langley Research Center

3. Technical University of Braunschweig

4. RWTH Aachen University

5. Arnold Engineering Development Complex

6. Sandia National Laboratories

7. University of Minnesota, Twin Cities

8. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0347

Reference40 articles.

1. Development of Hypersonic Quiet Tunnels

2. Aerothermodynamics and Transition in High-Speed Wind Tunnels at NASA Langley

3. Effect of wall cooling on boundary-layer-induced pressure fluctuations at Mach 6

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