The evolution of a two-dimensional, incompressible, rapidly decelerating, viscous flow about a sharp-edged camber is simulated through the use of discrete-vortex method. An extensive study of the velocity field in the vicinity of the singular points led to the development of a novel method for the introduction of vorticity. The roll-up of the vortex sheets, the distribution of velocity and the pressure on the camber, and the drag force are calculated and compared with experiments.
MOSTAFA, S. (1989). A DISCRETE-VORTEX ANALYSIS OF UNSTEADY FLOW ABOUT CAMBERED PLATES. International Conference on Aerospace Sciences and Aviation Technology, 3(ASAT Conference 4-6 April 1989 , CAIRO), 11-21. doi: 10.21608/asat.1989.25857
MLA
SAMIR I. M. MOSTAFA. "A DISCRETE-VORTEX ANALYSIS OF UNSTEADY FLOW ABOUT CAMBERED PLATES". International Conference on Aerospace Sciences and Aviation Technology, 3, ASAT Conference 4-6 April 1989 , CAIRO, 1989, 11-21. doi: 10.21608/asat.1989.25857
HARVARD
MOSTAFA, S. (1989). 'A DISCRETE-VORTEX ANALYSIS OF UNSTEADY FLOW ABOUT CAMBERED PLATES', International Conference on Aerospace Sciences and Aviation Technology, 3(ASAT Conference 4-6 April 1989 , CAIRO), pp. 11-21. doi: 10.21608/asat.1989.25857
VANCOUVER
MOSTAFA, S. A DISCRETE-VORTEX ANALYSIS OF UNSTEADY FLOW ABOUT CAMBERED PLATES. International Conference on Aerospace Sciences and Aviation Technology, 1989; 3(ASAT Conference 4-6 April 1989 , CAIRO): 11-21. doi: 10.21608/asat.1989.25857
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