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- W865514150 abstract "The effects of the inlet pressure distortions, induced by five screen patterns, on the performance of a J85-21 turbojet engine was conducted at the NASA Lewis Research Center. Testing was in support of the HiMAT RPRV program at Dryden Flight Research Center. Distortion patterns were chosen based on anticipated application of test results of the HiMAT installation. Tests were conducted at a simulated Mach number and altitude condition of 0.9 and 10 973 meters. Results are presented in terms of distortion levels and standard compressor performance parameters." @default.
- W865514150 created "2016-06-24" @default.
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- W865514150 date "1979-03-01" @default.
- W865514150 modified "2023-09-26" @default.
- W865514150 title "Effects of steady-state pressure distortion on the stall margin of a J85-21 turbojet engine" @default.
- W865514150 hasPublicationYear "1979" @default.
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