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Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds subsonic leading edges and supersonic trailing edges
Document ID
19930082532
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Malvestuto, Frank S , Jr
Margolis, Kenneth
Ribner, Herbert Spencer
Date Acquired
August 29, 2013
Publication Date
April 1, 1949
Report/Patent Number
NACA-TN-1860
Report Number: NACA-TN-1860
Accession Number
93R11822
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DAMPING IN ROLL
THEORIES - WINGS, SUPERSONIC
WINGS, SWEPTBACK - CHARACTERISTICS, EFFECT OF COMPRESSIBILITY
WINGS, SWEPTBACK - TAPERED
PRESSURE DISTRIBUTION - WINGS, SWEPTBACK
WINGS, THIN

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