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Cryogenic strain gage techniques used in force balance design for the National Transonic FacilityA force balance is a strain gage transducer used in wind tunnels to measure the forces and moments on aerodynamic models. Techniques have been established for temperature-compensation of force balances to allow their use over the operating temperature range of a cryogenic wind tunnel (-190C to 60C) without thermal control. This was accomplished by using a patented strain gage matching process to minimize inherent thermal differences, and a thermal compensation procedure to reduce the remaining thermally-induced outputs to acceptable levels. A method of compensating for mechanical movement of the axial force measuring beam caused by thermally-induced stresses under transient temperatures was also included.
Document ID
19860018146
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ferris, A. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-87712
NAS 1.15:87712
Report Number: NAS 1.15:87712
Report Number: NASA-TM-87712
Accession Number
86N27618
Funding Number(s)
PROJECT: RTOP 505-61-01-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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