Publication Date:
2016-06-07
Description:
The quasi vortex-lattice method is reviewed and applied to the evaluation of backwash, with applications to ground effect analysis. It is also extended to unsteady aerodynamics, with particular interest in the calculation of unsteady leading-edge suction. Some applications in ornithopter aerodynamics are given.
Keywords:
AERODYNAMICS
Type:
NASA. Langley Res. Center Vortex-Lattice Utilization; p 385-406
Format:
application/pdf