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Pressure distribution and damping in steady roll at supersonic Mach numbers of flat swept-back wing with subsonic edges
Document ID
19930082702
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Walker, Harold J
Ballantyne, Mary B
Date Acquired
August 16, 2013
Publication Date
March 1, 1950
Report/Patent Number
NACA-TN-2047
Report Number: NACA-TN-2047
Accession Number
93R11992
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROLLING MOMENTS - WINGS, SWEPTBACK
DAMPING IN ROLL
THEORIES - FLOW - SUPERSONIC
PRESSURE DISTRIBUTION - WINGS, SWEPTBACK
THEORIES - WINGS
WINGS, DELTA
THEORIES - FLOW - LINEAR
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