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Effect of thickness and sweep angle on the longitudinal aerodynamic characteristics of slab delta planforms at a Mach number of 20Effect of thickness and sweep angle on longitudinal aerodynamic characteristics of slab delta planforms at hypersonic speed
Document ID
19660019919
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marcum, D. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Witcofski, R. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3459
Report Number: NASA-TN-D-3459
Accession Number
66N29209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
HYPERSONIC SPEED
AERODYNAMIC CHARACTERISTICS
SWEEPBACK ANGLE
WING PLANFORM

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