Surface integral developed which yields solutions of linearized partial differential equation for supersonic flow; these solutions satisfy boundary conditions arising in wing theory; particular applications of this general method are made using acceleration potentials, to flat surface and to uniformly loaded lifting surfaces.
Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems
Nat Advisory Committee Aeronautics -- Tech Note
1947
56 pages
Bibliography, 21 Supp Sheets
Report
Englisch
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Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems
Engineering Index Backfile | 1947
|Second-order solution for oscillating two-dimensional supersonic airfoil
Engineering Index Backfile | 1952
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