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Development of a pressure and force transducer calibration procedure for the hypersonic shock tunnel, volume I Final report, May 1963 - Oct. 1966Investigation of pressure transducers, sound pressure generation systems, pressure transducer mounting, and forced oscillation dynamic balance for application to hypersonic shock tunnel
Document ID
19670008673
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Loyd, J. R. (Astro-Space Labs., Inc. Huntsville, AL, United States)
Pickard, R. F. (Astro-Space Labs., Inc. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
January 17, 1967
Subject Category
Instrumentation And Photography
Report/Patent Number
ER67-2, VOL. I
NASA-CR-81713
Report Number: ER67-2, VOL. I
Report Number: NASA-CR-81713
Accession Number
67N18002
Funding Number(s)
CONTRACT_GRANT: NAS8-5350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FORCED OSCILLATION
BALANCE
PRESSURE TRANSDUCER
HYPERSONIC WIND TUNNEL

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