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A New Correction Technique for Strain-Gage Measurements Acquired in Transient-Temperature EnvironmentsSignificant strain-gage errors may exist in measurements acquired in transient-temperature environments if conventional correction methods are applied. As heating or cooling rates increase, temperature gradients between the strain-gage sensor and substrate surface increase proportionally. These temperature gradients introduce strain-measurement errors that are currently neglected in both conventional strain-correction theory and practice. Therefore, the conventional correction theory has been modified to account for these errors. A new experimental method has been developed to correct strain-gage measurements acquired in environments experiencing significant temperature transients. The new correction technique has been demonstrated through a series of tests in which strain measurements were acquired for temperature-rise rates ranging from 1 to greater than 100 degrees F/sec. Strain-gage data from these tests have been corrected with both the new and conventional methods and then compared with an analysis. Results show that, for temperature-rise rates greater than 10 degrees F/sec, the strain measurements corrected with the conventional technique produced strain errors that deviated from analysis by as much as 45 percent, whereas results corrected with the new technique were in good agreement with analytical results.
Document ID
19960016591
Acquisition Source
Headquarters
Document Type
Technical Publication (TP)
Authors
Richards, W. Lance
(NASA Dryden Flight Research Center Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TP-3593
H-2043
NAS 1.60:3593
Report Number: NASA-TP-3593
Report Number: H-2043
Report Number: NAS 1.60:3593
Accession Number
96N22235
Funding Number(s)
PROJECT: RTOP 505-70-63
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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