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Experimentally determined local flow properties and drag coefficients for a family of blunt bodies at Mach numbers from 2.49 to 4.63Experimentally determined local flow properties and drag coefficients for family of blunt bodies at Mach numbers from 2.49 to 4.63
Document ID
19670030271
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Stallings, R. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TR-R-274
Report Number: NASA-TR-R-274
Accession Number
67N39600
Funding Number(s)
CONTRACT_GRANT: 124-07-02-44-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DRAG COEFFICIENT
FLOW MEASUREMENT
BLUNT BODY
SUPERSONIC FLOW

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