Entry, Descent and Landing Aerothermodynamics: NASA Langley Experimental Capabilities and Contributions-Reference-Cited by-同舟云学术

Entry, Descent and Landing Aerothermodynamics: NASA Langley Experimental Capabilities and Contributions

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
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Author:

Hollis Brian R.¹,Berger Karen T.¹,Berry Scott A.¹,Brauckmann Greg J.¹,Buck Gregory M.¹,DiFulvio Michael¹,Horvath Thomas J.¹,Liechty Derek S.¹,Merski N. R.¹,Murphy Kelly J.¹,Rufer Shann J.¹,Schoenenberger Mark¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-1154

Reference78 articles.

1. Langley Aerothermodynamic Facilities Complex - Enhancements and testing capabilities

2. Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center - Aerothermodynamic Facilities Complex

3. Langley Research Center's Unitary Plan Wind Tunnel - Testing capabilities and recent modernization activities

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