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Measuring unsteady pressure on rotating compressor bladesMiniature semiconductor strain gage pressure transducers mounted in several arrangements were studied. Both surface mountings and recessed flush mountings were tested. Test parameters included mounting arrangement, blade material, temperature, local strain in the acceleration normal to the transducer diaphragm, centripetal acceleration, and pressure. Test results show no failures of transducers or mountings and indicate an uncertainty of unsteady pressure measurement of approximately + or - 6 percent + 0.1 kPa for a typical application. Two configurations were used on a rotating fan flutter program. Examples of transducer data and correction factors are presented.
Document ID
19790014277
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Englund, D. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Grant, H. P.
(Pratt and Whitney Aircraft East Hartford, Conn., United States)
Lanati, G. A.
(Pratt and Whitney Aircraft East Hartford, Conn., United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-79159
E-015
Report Number: NASA-TM-79159
Report Number: E-015
Meeting Information
Meeting: Intern. Instrumentation Symp.
Location: Anaheim, Calif.
Country: United States
Start Date: May 7, 1979
End Date: May 10, 1979
Sponsors: Instr. Soc. of Am.
Accession Number
79N22448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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