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Rolling and yawing moments for swept-back wings in sideslip at supersonic speeds
Document ID
19930082927
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lampert, Seymour
Date Acquired
August 29, 2013
Publication Date
January 1, 1951
Report/Patent Number
NACA-TN-2262
Report Number: NACA-TN-2262
Accession Number
93R12217
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LINEAR
ROLLING & YAWING MOMENTS - WINGS, SWEPTBACK
THEORIES - WINGS
THEORIES - FLOW
ROLLING MOMENTS - EFFECT OF SIDESLIPPING
SUPERSONIC
YAWING MOMENTS - EFFECT OF SIDESLIPPING
CONICAL
WINGS, SWEPTBACK - TAPERED
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