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Effect of aspect ratio and taper on the pressure drag at supersonic speeds of unswept wings at zero lift
Document ID
19930082144
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Nielsen, Jack N
Date Acquired
August 16, 2013
Publication Date
November 1, 1947
Report/Patent Number
NACA-TN-1487
Report Number: NACA-TN-1487
Accession Number
93R11434
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS, WEDGE - DOUBLE
THEORIES - FLOW SOURCES & SINKS
WINGS, RECTANGULAR
PRESSURE DISTRIBUTION - WINGS
WINGS, TAPERED
THEORIES - FLOW, SUPERSONIC
DRAG - WINGS
THEORIES - FLOW LINEAR
AIRFOILS - ASPECT RATIO
WINGS,DIAMOND
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