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Component Performance Investigation of J71 Experimental Turbine. Iv-effect of First-stator Adjustment; Over-all Performance of J71-97 Turbine with 132-percent-design Stator AreaAn experimental invesitgation of the effect of increasing the first-stator area of the J71-97 experimental three-stage turbine from 97 percent of design to 132 percent revealed (1) the maximum efficiency obtained decreased from 0.891 to 0.869, (2) the choking equivalent weight flows increased by approximately 13.6 percent, and (3) at the turbine match points required to maintain the compressor at constant design equivalent conditions the turbine efficiency decreased from 0.87 to 0.86.
Document ID
19930094386
Acquisition Source
Legacy CDMS
Document Type
None
Authors
Davison, Elmer H
Petrash, Donald A
Schum, Harold J
Date Acquired
August 16, 2013
Publication Date
April 17, 1956
Report/Patent Number
NACA RM E55H09
Report Number: NACA RM E55H09
Accession Number
93R23305
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBINES -ALLISON J-71
TURBINES-AXIAL-FLOW
FLOW - TURBINES
ENGINES, TURBOJET
TURBINE FLOW THEORY AND EXPERIMENT
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