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Theoretical characteristics in supersonic flow of constant-chord partial-span control surfaces on rectangular wings having finite thickness
Document ID
19930082397
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tucker, Warren A
Nelson, Robert L
Date Acquired
August 16, 2013
Publication Date
September 1, 1948
Report/Patent Number
NACA-TN-1708
Report Number: NACA-TN-1708
Accession Number
93R11687
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, RECTANGULAR
THEORIES - FLOW - BUSEMANN
CONTROL SURFACES - EFFECT OF COMPRESSIBILITY
CONTROL SURFACES - HINGE MOMENTS
CONTROL SURFACES - CHARACTERISTICS
THEORIES - FLOW SUPERSONIC
THEORIES - FLOW LINEAR
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