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Component Performance Investigation of J71 Experimental Turbine VII: Effect of First-stator Adjustment; Over-all Performance of J71-97 Turbine with 87-percent-design Stator AreaThe performance results, as well as a compressor-turbine match point study based on a particular mode of engine operation, are compared with those previously obtained with the same turbine having first-stator areas 70, 95.6, and 132 percent of design. Maximum efficiencies for all turbine configurations were high, on the order of 87 to 89 percent. The efficiencies obtained at the match points for the 87-, 95.6-, and 132-percent turbines were slightly lower. No match point for the 70-percent turbine was obtained because, with first-stator areas less than 75.5 percent of design, the turbine would develop insufficient work to drive the compressor at the match point.
Document ID
19930089343
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Schum, Harold J
Petrash, Donald A
Davison, Elmer H
Date Acquired
August 16, 2013
Publication Date
January 14, 1957
Report/Patent Number
NACA-RM-E56F20
Report Number: NACA-RM-E56F20
Accession Number
93R18633
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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