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Wind-tunnel calibration of a 40 deg conical pressure probe at Mach numbers from 3.5 to 7.4Wind tunnel calibration of conical pressure probe over range of Mach numbers to determine flow field data for X-15 airplane
Document ID
19680019329
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Burcham, F. W., Jr. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-4678
Report Number: NASA-TN-D-4678
Accession Number
68N28801
Funding Number(s)
CONTRACT_GRANT: 729-00-00-02-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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