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Steady-state performance of J85-21 compressor at 100 percent of design speed with and without interstage rake blockageInternal compressor instrumentation blockage effects on steady state J85-21 compressor performance at 100 percent of design speed are determined. The blockage was generated by instrumented vanes for the first three compressor stages and by removal rakes for stages 4 to 9. Individual flow passage blockages ranged up to 4.5 percent with the instrumented vanes and up to 22 percent with the removable interstage rakes. At a Reynolds number index of 1.0, pressure ratio and airflow remained unchanged with insertion of the interstage rakes, but efficiency dropped 0.3 percentage point. Compressor exit profiles, compressor stage static pressure rise coefficients, turbine exit temperature, and fuel flow are also presented.
Document ID
19800012848
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Werner, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-377
NASA-TM-81451
Report Number: E-377
Report Number: NASA-TM-81451
Accession Number
80N21333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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