Fighter Aircraft Synthesis/Design Optimization
This thesis presents results of the application of energy-based large-scale optimization of a two-subsystem (propulsion subsystem (PS) and airframe subsystem-aerodynamics (AFS-A)) air-to-air fighter (AAF) with two types of AFS-A models: a fixed-wing AFS-A and a morphing-wing AFS-A. The AAF flies 19...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/32821 http://scholar.lib.vt.edu/theses/available/etd-05152009-125049/ |