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THE AERODYNAMIC CHARACTERISTICS OF A BODY IN THE FLOW FIELD NEAR THE TIP OF A CIRCULAR-ARC WING OF RECTANGULAR PLAN FORM AT A MACH NUMBER OF 2.01Aerodynamic characteristics of body in flow field near tip of circular-arc wing of rectangular planform at mach 2.01
Document ID
19630003039
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gapcynski, J. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1960
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TM-X-211
Report Number: NASA-TM-X-211
Accession Number
63N12915
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING
SUPERSONIC SPEED
AERODYNAMIC CHARACTERISTICS
FLOW FIELD

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