NASA NTRS · 20050028483
Two-Dimensional Wing Theory in the Supersonic Range
Abstract
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.
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Hoenl, H.. 1949-06-01. Two-Dimensional Wing Theory in the Supersonic Range. https://ntrs.nasa.gov/citations/20050028483
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