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Visualization of unsteady separated flow about a pitching delta wing
1987
25th AIAA Aerospace Sciences Meeting
unpublished
ELf C-T D.istribution Unlimited , Unsteady separated flows produced by three different delta wings driver with constant pitch rates were investigated using high speed flow visualization. The large scale vortices produced were initially similar to those produced above delta wings driven sinusoidally. Subsequently, the vortices either convected away from the wing or were broken up by the complex three-dimensional flow field. Both initiation and development of the leading edge vortices were
doi:10.2514/6.1987-240
fatcat:pmon2nwywjggnbw6dhp4e4mhh4