Problems of Transient lift on two- and three-dimensional wings flying at high speeds discussed as boundary value problem for classical wave equation; Kirchhoff's formula is applied so that analysis is reduced, just as in steady state, to investigation of sources and doublets. Supersedes NACA -- Tech Notes 2403 and 2387.
Two- and three-dimensional unsteady lift problems in high-speed flight
NACA -- Report
1952
55 pages
Bibliography
Report
English
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Three-dimensional, unsteady-lift problems in high-speed flight -- Basic concepts
Engineering Index Backfile | 1950
|Three-dimensional unsteady lift problems in high-speed flight -- Triangular wing
Engineering Index Backfile | 1951
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