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Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds.subsonic leading edges
Document ID
19930082719
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Margolis, Kenneth
Date Acquired
August 16, 2013
Publication Date
March 1, 1950
Report/Patent Number
NACA-TN-2048
Report Number: NACA-TN-2048
Accession Number
93R12009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIFT - WINGS, SWEPTBACK
DAMPING IN ROLL
AIRFOILS - THICKNESS
THEORIES - WING - SUPERSONIC
THEORIES - FLOW - LINEAR
WING TIPS - SHAPES
WINGS, SWEPTBACK - TAPERED
WING TIPS, RAKED
WINGS, SWEPTBACK - STABILITY

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