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Two-Dimensional Wing Theory in the Supersonic RangeThe 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.
Document ID
20050028483
Acquisition Source
Langley Research Center
Document Type
Other - NACA Technical Memorandum
Authors
Hoenl, H. (Zentrale fuer Wissenschaftliches Berichtswesen Berlin, Germany)
Date Acquired
August 22, 2013
Publication Date
June 1, 1949
Publication Information
Publication: ZWB Forschungsbericht Nr. 1903
Subject Category
Aerodynamics
Report/Patent Number
NACA-TM-1238
Report Number: NACA-TM-1238
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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