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Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
Document ID
19930089773
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moore, John A
Date Acquired
August 29, 2013
Publication Date
September 19, 1957
Report/Patent Number
NACA-RM-L57G10a
Report Number: NACA-RM-L57G10a
Accession Number
93R19063
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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