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Strain sensing technology for high temperature applicationsThis review discusses the status of strain sensing technology for high temperature applications. Technologies covered are those supported by NASA such as required for applications in hypersonic vehicles and engines, advanced subsonic engines, as well as material and structure development. The applications may be at temperatures of 540 C (1000 F) to temperatures in excess of 1400 C (2500 F). The most promising technologies at present are the resistance strain gage and remote sensing schemes. Resistance strain gages discussed include the BCL gage, the LaRC compensated gage, and the PdCr gage. Remote sensing schemes such as laser based speckle strain measurement, phase-shifling interferometry, and x-ray extensometry are discussed. Present status and limitations of these technologies are presented.
Document ID
19940008401
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, W. Dan
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1993
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-4498
E-7650
NAS 1.26:4498
Report Number: NASA-TM-4498
Report Number: E-7650
Report Number: NAS 1.26:4498
Meeting Information
Meeting: AIAA International Aerospace Planes Conference
Location: Orlando, FL
Country: United States
Start Date: December 1, 1992
End Date: December 4, 1992
Accession Number
94N12874
Funding Number(s)
PROJECT: RTOP 505-62-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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