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Supersonic flow past oscillating airfoils including nonlinear thickness effects
Document ID
19930083707
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Van Dyke, Milton D
Date Acquired
August 16, 2013
Publication Date
July 1, 1953
Report/Patent Number
NACA-TN-2982
Report Number: NACA-TN-2982
Accession Number
93R12997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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