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

Author:

JingBo Yu1,Wang Hongwei1,Xiang Xingju1

Affiliation:

1. China Academy of Aerospace Aerodynamics

Publisher

American Institute of Aeronautics and Astronautics

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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