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A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 DegHigh angle aerodynamic characteristics produced by nose cone of revolution in wind tunnel at supersonic speed
Document ID
19650014315
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Smith, F. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-311
Report Number: NASA-TM-X-311
Accession Number
65N23916
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOSE CONE
SUPERSONIC WIND TUNNEL
SUPERSONIC SPEED
AERODYNAMIC CHARACTERISTICS

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