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Parallel solution of low aspect ratio rectangular flat wings in compressible flow
(2005)
Two block parallel Navier Stokes solutions of an aspect ratio 1.0 flat plate with sharp edges are obtained at different Mach numbers and angles of attack. Reynolds numbers are of the order of 200,000-300,000. The flow field ...
Open and closed loop control of a transport aircraft after component failure
(2011)
Aircraft dynamics are severely affected by the damages and failures of components. If corrective commands are not supplied immediately, force and moment imbalances lead into catastrophic consequences. In this study, flight ...