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Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration.Subsonic leading edges and supersonic trailing edges
Document ID
19930082993
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Malvestuto, Frank S , Jr
Hoover, Dorothy M
Date Acquired
August 29, 2013
Publication Date
March 1, 1951
Report/Patent Number
NACA-TN-2315
Report Number: NACA-TN-2315
Accession Number
93R12283
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION - WINGS, SWEPTBACK
WINGS, THIN
PITCHING MOMENTS - WINGS, SWEPTBACK
WINGS - ASPECT RATIO
WINGS, SWEPTBACK - CHARACTERISTICS
WINGS, SWEPTBACK - TAPERED
SUPERSONIC
EFFECT OF COMPRESSIBILITY
THEORIES - WINGS
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