Development of Methods for Improved Data Integrity and Efficient Testing of Wind Tunnel Models for Dynamic Test Conditions in Unsteady and Nonlinear Flight Regimes
Todayâ s high performance aircraft are operating in expanded flight envelopes, often maneuvering at high angular rates at high angles-of-attack, even above maximum lift. Current aerodynamic models are inadequate in predicting flight characteristics in the expanded envelope, such as rapid aircraft d...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/31050 http://scholar.lib.vt.edu/theses/available/etd-01272004-110610/ |