Large-Amplitude High-Rate Roll Experiments on a Delta and Double Delta Wing
نویسنده
چکیده
A comprehensive wind-tunnel test program on both a 65o delta an 80o/65o double delta wing model has been recently completed. The program included static and dynamic force tests. A brief description of the various experiments is presented, as well as results that demonstrate the value of the previously proposed "hypersurface" representation of aerodynamic loads in the non-linear and unsteady regimes.
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