Analysis and Comparison of Effects of an Airfoil or a Rod on Supersonic Cavity Flow.
The effects of an airfoil at different angles of attack and a circular cylindrical rod within the edge of the boundary layer flow at the leading edge of a cavity as a device for controlling the large pressure fluctuations (resonance tones) in the cavity were investigated. The airfoil results were co...
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| Format: | Others |
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Trace: Tennessee Research and Creative Exchange
2010
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| Online Access: | http://trace.tennessee.edu/utk_gradthes/796 |