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Experimental stability and drag of a pointed and a blunted 30 deg half-angle cone at Mach numbers from 11.5 to 34 in airStatic and dynamic stability and drag of blunted and pointed cones at various Mach numbers and Reynolds numbers
Document ID
19660005467
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Intrieri, P. F. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3193
Report Number: NASA-TN-D-3193
Accession Number
66N14756
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MACH NUMBER
DYNAMIC STABILITY
CONE
REYNOLDS NUMBER
DRAG COEFFICIENT
STATIC STABILITY

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