Unsteady Pressure Measurement of Cavity Flow In a Hypersonic Wind Tunnel Using Fast Response PSP-Reference-Cited by-同舟云学术

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Unsteady Pressure Measurement of Cavity Flow In a Hypersonic Wind Tunnel Using Fast Response PSP

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
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Author:

JingBo Yu¹,Wang Hongwei¹,Xiang Xingju¹

Affiliation:

1. China Academy of Aerospace Aerodynamics

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2209

Reference16 articles.

1. Rossiter J E. Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds [R]. Aeronautical ReaearchCouncil Reports andMemoranda, Technical Reports3438,1964

2. Heller H, Bliss D. Aerodynamically Induced Pressure Oscillations in Cavities. Physical Mechanisms and Suppression Concepts.1975, AFFDLTR-74-133

3. On the tones and pressure oscillations induced by flow over rectangular cavities

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