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Load distributions due to steady roll and pitch for thin wings at supersonic speeds
Document ID
19930082327
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moeckel, W E
Evvard, J C
Date Acquired
August 16, 2013
Publication Date
August 1, 1948
Report/Patent Number
NACA-TN-1689
Report Number: NACA-TN-1689
Accession Number
93R11617
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - FLOW SUPERSONIC
THEORIES - WINGS
LOAD DISTRIBUTION - WINGS
WINGS - STABILITY
AIRFOILS,THIN
ROLLING & PITCHING MOMENTS
LIFT DISTRIBUTION - WINGS
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