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Low-speed tests of 50 deg-swept parawings applied to a 0.17-scale model of a manned flight vehicleShock wave interference and degradation in wind tunnel caused by protruding teeth, recessions, local expansions, and combinations of these
Document ID
19660022569
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bugg, F. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3493
Report Number: NASA-TN-D-3493
Accession Number
66N31859
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPT WING
LOW SPEED WIND TUNNEL
FLIGHT VEHICLE

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