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Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube
Document ID
19930093487
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Humphreys, Milton D
Date Acquired
September 6, 2013
Publication Date
April 1, 1945
Report/Patent Number
NACA-WR-L-77
NACA-RB-L5C30
Report Number: NACA-WR-L-77
Report Number: NACA-RB-L5C30
Accession Number
93R22777
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INSTRUMENTS-PITOT TUBES
PRESSURE-EFFECT OF COMPRESSIBILITY & ANGLE OF YAW
WIND TUNNEL TESTS-NACA-HIGH-SPEED (18 INCHES X 4 INCHES)

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