Measurements of Resonance in a Forward-Facing Cavity at Mach Six-Reference-Cited by-同舟云学术

Measurements of Resonance in a Forward-Facing Cavity at Mach Six

Published:2015-09 Issue:5 Volume:52 Page:1486-1494
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Chou Amanda¹,Schneider Steven P.²

Affiliation:

1. Research Aerospace Engineer, NASA Langley Research Center, Hampton, Virginia 23681

2. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47907

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33286

Reference29 articles.

1. StallingsR. L.Jr.BurbankP. B. “Heat-Transfer and Pressure Measurements on a Concave-Nose Cylinder for a Mach Number Range of 2.49 to 4.44,” NASA TR-TM-X-221, Oct. 1959.

2. Mach 10 bow-shock behavior of a forward-facing nose cavity

3. Unsteady flowfield over a forward-looking endoatmospheric hit-to-kill interceptor

4. Nose cavity effects on blunt body pressure and temperatures at Mach 5

5. Fluid Dynamics of Hypersonic Forward-Facing Cavity Flow

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