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Demonstration test of burner liner strain measurements using resistance strain gagesA demonstration test of burner liner strain measurements using resistance strain gages as well as a feasibility test of an optical speckle technique for strain measurement are presented. The strain gage results are reported. Ten Kanthal A-1 wire strain gages were used for low cycle fatigue strain measurements to 950 K and .002 apparent strain on a JT12D burner can in a high pressure (10 atmospheres) burner test. The procedure for use of the strain gages involved extensive precalibration and postcalibration to correct for cooling rate dependence, drift, and temperature effects. Results were repeatable within + or - .0002 to .0006 strain, with best results during fast decels from 950 K. The results agreed with analytical prediction based on an axisymmetric burner model, and results indicated a non-uniform circumferential distribution of axial strain, suggesting temperature streaking.
Document ID
19870001757
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grant, H. P.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Anderson, W. L.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Turbine Engine Hot Section Technology, 1984
Subject Category
Instrumentation And Photography
Accession Number
87N11190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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