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Shock-swallowing air sensorAn air-data probe allows air to flow through it so that supersonic and hypersonic shock waves form behind pressure measuring orifices and tube instead of directly on them. Measured pressures are close to those in free-flowing air and are used to determine mach numbers of flying aircraft.
Document ID
19780000537
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Nugent, J. (Langley Res. Center)
Sakamoto, G. M.
Webb, L. D.
Couch, L. M.
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
FRC-10107
Accession Number
78B10537
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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