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The effects of yawing thin pointed wings at supersonic speeds
Document ID
19930082174
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Evvard, John C
Date Acquired
August 16, 2013
Publication Date
September 1, 1947
Report/Patent Number
NACA-TN-1429
Report Number: NACA-TN-1429
Accession Number
93R11464
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIFT & DRAG - WINGS, DELTA
THEORIES - FLOW SUPERSONIC
WINGS - LEADING EDGES, ROUNDED
DRAG, WAVE
AIRFOILS, THIN
CENTER OF PRESSURE - WINGS, DELTA
ROLLING MOMENTS - WINGS, DELTA
PRESSURE DISTRIBUTION - WINGS, DELTA
WINGS, DELTA - YAWED
THEORIES - WINGS
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