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Pressure distribution and damping in steady pitch at supersonic Mach numbers of flat swept-back wings having all edges subsonic
Document ID
19930082846
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Walker, Harold J
Ballantyne, Mary B
Date Acquired
August 16, 2013
Publication Date
October 1, 1950
Report/Patent Number
NACA-TN-2197
Report Number: NACA-TN-2197
Accession Number
93R12136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, FLAT
SUPERSONIC
WINGS, SWEPTBACK - STABILITY, LONGITUDINAL
CONICAL
LINEAR
WING TIPS
THEORIES - FLOW
DAMPING IN PITCH
PRESSURE DISTRIBUTION - WINGS, SWEPTBACK
THEORIES - WINGS
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