Pressure distribution over thin airfoil of infinite span is calculated by integrating disturbances due to appropriate distribution of sources over forepart of Mach cone for point at which pressure is desired; result expressed in terms of Green's function giving pressure at any point on airfoil due to unit harmonic velocity at any other point. (correction) n 11 Nov p 630.
Aerodynamic forces on oscillating airfoil at supersonic speeds
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 14 , n 6
1947
8 pages
Article (Journal)
English
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Aerodynamic center and center of pressure of airfoil at supersonic speeds
Engineering Index Backfile | 1947
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NTIS | 1971
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