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Strain sensing technology for high temperature applicationsThis review paper 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-shifting interferometry and X-ray extensometry will be discussed. Present status and limitations of these technologies are presented.
Document ID
19930038317
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Williams, W. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
December 1, 1992
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 92-5040
Report Number: AIAA PAPER 92-5040
Meeting Information
Meeting: AIAA, International Aerospace Planes Conference
Location: Orlando, FL
Country: United States
Start Date: December 1, 1992
End Date: December 4, 1992
Sponsors: AIAA
Accession Number
93A22314
Distribution Limits
Public
Copyright
Other

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