Following methods introduced by J. HADAMARD, solution to thin airfoil problem in supersonic theory is given in terms of distribution of sources and doublets over given reference plane; nature of boundary values required discussed.
Use of source-sink and doublet distributions extended to solution of arbitrary boundary value problems in supersonic flow
Nat Advisory Committee Aeronautics -- Tech Note
1948
48 pages
Article (Journal)
English
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Engineering Index Backfile | 1948
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