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Estimation of the damping in roll of supersonic-leading-edge wing-body combinations
Document ID
19930082769
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tucker, Warren A
Piland, Robert O
Date Acquired
August 16, 2013
Publication Date
July 1, 1950
Report/Patent Number
NACA-TN-2151
Report Number: NACA-TN-2151
Accession Number
93R12059
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INTERFERENCE - WINGS & BODIES
DAMPING IN ROLL
WINGS, DELTA
THEORIES - FLOW - SUPERSONIC
THEORIES - FLOW - LINEAR
FUSELAGE-WING COMBINATIONS
WINGS, RECTANGULAR
THEORIES - WINGS - SUPERSONIC
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