Development and Use of a Computer Program “Hyper-N” to Predict the Performance of Air Vehicles Traveling at Hypersonic Speeds
Abstract The main objective of this thesis was to develop a method than can be used to approximate the pressure forces on air vehicles traveling at hypersonic speed (Mach number > 5). The aerodynamic forces such as lift and drag were calculated from the pressure values on the surface of the airpl...
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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/684 |