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The Effect of Camber on the Aerodynamic Characteristics of a Body at a Mach Number of 2.01Effect of camber on aerodynamic characteristics of ogive-circular-cylindrical body at mach 2.01
Document ID
19630003232
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gapcynski, J. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
September 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-56
Accession Number
63N13108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CAMBER
CYLINDER
AERODYNAMIC CHARACTERISTICS
SUPERSONIC SPEED
CIRCULAR CYLINDER

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