Results 271 to 280 of about 332,136 (301)
Some of the next articles are maybe not open access.
1973
Abstract : A theoretical description is presented on the experimentally observed phenomenon of wing leading-edge vortex lift control by spanwise mass injection. The vortex and jet initial source/sink strengths and locations are established by a conformal mapping solution, and used as starting conditions for an iterative vortex-lattice simulation.
Charles J. Dixon +2 more
openaire +1 more source
Abstract : A theoretical description is presented on the experimentally observed phenomenon of wing leading-edge vortex lift control by spanwise mass injection. The vortex and jet initial source/sink strengths and locations are established by a conformal mapping solution, and used as starting conditions for an iterative vortex-lattice simulation.
Charles J. Dixon +2 more
openaire +1 more source
UNSTEADY LIFT PRODUCED BY A STREAMWISE VORTEX IMPINGING ON AN AIRFOIL
Journal of Fluids and Structures, 2002Abstract An analytical model is investigated to estimate the spectrum of the unsteady lift produced by a low Mach number, streamwise vortex “playing” on the leading edge of a thin airfoil. The vortex is assumed to exhibit a random wave-like behavior induced by mean flow turbulence and upstream influence from the edge, and to contain quasi-periodic ...
openaire +1 more source
Vortex Lift Waverider Configurations
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012openaire +1 more source
Vortex induced transient separation on a lifting surface
32nd Aerospace Sciences Meeting and Exhibit, 1994R. Funk +3 more
openaire +1 more source
Vortex-lift prediction for complex wing planforms.
Journal of Aircraft, 1973R. G. Bradley +2 more
openaire +1 more source
Implications of the Insensitivity of Vortex Lift to Sweep
Journal of Aircraft, 2000openaire +1 more source