Mach 8 High Reynolds Number Static Stability Capability Extension Using a Hypersonic Waverider at AEDC Tunnel 9-Reference-Cited by-同舟云学术

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Mach 8 High Reynolds Number Static Stability Capability Extension Using a Hypersonic Waverider at AEDC Tunnel 9

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
language:
Short-container-title:

Author:

Norris Joseph¹

Affiliation:

1. AEDC White Oak

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2815

Reference11 articles.

1. 1Kammeyer, M., and Gillum, M., Design Validation Tests on a Realistic Hypersonic Waverider at Mach 10, 14, and 16.5 in the NavalSurface Warefare Center Hypervelocity Wind Tunnel No. 9, NSWCDD/TR-93/198,5 May1994,Silver Spring, MD.

2. CFD Analysis of a Generic Waverider

3. Numerical Simulation of the AEDC Waverider at Mach 8

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2. Extension of the Simple Analytical Model for Waverider Design;Journal of Spacecraft and Rockets;2018-07

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