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PARAWING AERODYNAMICSApplication of the tension structure concept for flexible wings to be used in spacecraft recovery and landing, emphasizing para-wing aerodynamics
Document ID
19630021500
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Johnson, J. L., Jr.
Sleeman, W. C., Jr.
Date Acquired
August 1, 2013
Publication Date
June 1, 1963
Subject Category
Auxiliary Systems
Accession Number
63A17559
Distribution Limits
Public
Copyright
Other
Keywords
FLEXIBLE WING
PARAGLIDER
AERODYNAMIC CHARACTERISTICS

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