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Miniature Flow-Direction/Pitot-Static Pressure ProbesPrecision flow-direction/pitot-static pressure probes, ranging from 0.035 to 0.090 inch (0.89 to 2.29 mm) in outside diameter, successfully fabricated and calibrated for use in Langley 20-inch Mach 6 Tunnel. Probes simultaneously measure flow direction and static and pitot pressures in flow fields about configurations in hypersonic flow at temperatures up to 500 degree F (260 degree C).
Document ID
19890000134
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Ashby, George C., Jr. (NASA Langley Research Center, Hampton, VA.)
Coombs, David S. (NASA Langley Research Center, Hampton, VA.)
Eves, John W. (NASA Langley Research Center, Hampton, VA.)
Price, Howard E. (NASA Langley Research Center, Hampton, VA.)
Vasquez, Peter (NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
March 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13643
Accession Number
89B10134
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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