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Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness
Document ID
19930082302
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Margolis, Kenneth
Date Acquired
August 16, 2013
Publication Date
August 1, 1948
Report/Patent Number
NACA-TN-1672
Report Number: NACA-TN-1672
Accession Number
93R11592
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS, WEDGE - DOUBLE
WINGS, SWEPTBACK - TAPERED
THEORIES - FLOW SUPERSONIC
THEORIES - FLOW SOURCES & SINKS
DRAG - WINGS
THEORIES - FLOW LINEAR
AIRFOILS - THICKNESS
DRAG, WAVE

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