The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.
Two-Dimensional Wing Theory in the Supersonic Range
1949-06-01
Miscellaneous
No indication
English
Two-dimensional wing theory in supersonic range
Engineering Index Backfile | 1949
|Two-dimensional wing theory in the supersonic range
TIBKAT | 1949
|Two-dimensional supersonic wing theory
NTRS | 1948
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TIBKAT | 1969
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AIAA | 1986
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