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Hutchison, Matthew Gerry
An approach to aerodynamic configuration optimization is presented for the high-speed civil transport (HSCT). Methods to parameterize the wing shape, fuselage shape and nacelle placement are described. Variable-complexity design strategies are used t
Externí odkaz:
http://hdl.handle.net/10919/38346
http://scholar.lib.vt.edu/theses/available/etd-06062008-165715/
http://scholar.lib.vt.edu/theses/available/etd-06062008-165715/