An experimental investigation of oblique wing static aeroelastic phenomena
A series of wind tunnel tests were conducted to determine the aerodynamic forces and moments produced by several clamped oblique wings. The wing sweep and aileron deflection angles were varied throughout a wide range of dynamic pressures. The wing structure was also stiffened. Strains were measured...
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| Format: | Others |
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/42938 http://scholar.lib.vt.edu/theses/available/etd-06082010-020326/ |