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Theoretical supersonic characteristics of inboard trailing-edge flaps having arbitrary sweep and taper : Mach lines behind flap leading and trailing edges
Document ID
19930082853
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kainer, Julian H
Marte, Jack E
Date Acquired
August 16, 2013
Publication Date
October 1, 1950
Report/Patent Number
NACA-TN-2205
Report Number: NACA-TN-2205
Accession Number
93R12143
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL SURFACES - EFFECT OF SWEEPBACK
CONTROL SURFACES - HINGE MOMENTS
CONTROL SURFACES - CHARACTERISTICS
THEORIES - FLOW, LINEAR
THEORIES - FLOW, SUPERSONIC

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