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AN INVESTIGATION AT SUBSONIC SPEEDS OF AERODYNAMIC CHARACTERISTICS AT ANGLES OF ATTACK FROM -4 DEG TO 100 DEG OF A DELTA-WING REENTRY CONFIGURATION HAVING FOLDING WINGTIP PANELSSubsonic aerodynamic characteristics of delta- wing reentry vehicle with folding wingtip panels
Document ID
19630003042
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spencer, B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-288
Report Number: NASA-TM-X-288
Accession Number
63N12918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
SUBSONIC FLOW
AERODYNAMIC CHARACTERISTICS
REENTRY VEHICLE

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