Methods of solution given for two- and three-dimensional steady state and two-dimensional unsteady state equations of compressible flow.
Application of green's theorem to solution of boundary-value problems in linearized supersonic wing theory
Nat Advisory Committee Aeronautics -- Tech Note
1949
41 pages
Diagrams, Photographs, Bibliography
Report
English
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Engineering Index Backfile | 1950
|Lift-cancellation technique in linearized supersonic-wing theory
Engineering Index Backfile | 1951
|Lift-cancellation technique in linearized supersonic-wing theory
TIBKAT | 1950
|