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REYNOLDS NUMBER EFFECTS ON THE INDUCED PRESSURES OF CYLINDRICAL BODIES WITH DIFFERENT NOSE SHAPES AND NOSE DRAG COEFFICIENTS IN HELIUM AT A MACH NUMBER OF 24Reynolds number effect on inviscid pressure distributions & shock shapes of cylindrical bodies with different nose shapes & drag coefficients
Document ID
19630013806
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Wagner, R. D., Jr. (NASA Langley Research Center Hampton, VA, United States)
WATSON R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TR-R-182
Report Number: NASA-TR-R-182
Accession Number
63N23686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK
PRESSURE DISTRIBUTION
DRAG COEFFICIENT
REYNOLDS NUMBER

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