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Low-subsonic wind-tunnel and free-flight drop-test investigation of a paraglider configuration having large tapered leading edges and keelLow subsonic wind tunnel and free flight drop test investigation of paraglider with large inflatable tapered leading edges and keel
Document ID
19660028846
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Croom, D. P. (NASA Langley Research Center Hampton, VA, United States)
Fournier, P. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3442
Report Number: NASA-TN-D-3442
Accession Number
66N38136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
DROP TEST
PARAGLIDER
SUBSONIC WIND TUNNEL
INFLATABLE GLIDER

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