Effects of Active and Passive Control Techniques on Mach 1.5 Cavity Flow Dynamics
Supersonic flow over cavities has been of interest since 1960s because cavities represent the bomb bays of aircraft. The flow is transient, turbulent, and complicated. Pressure fluctuations inside the cavity can impede successful weapon release. The objective of this study is to use active and passi...
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Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
Wiley
2017-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2017/8253264 |
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