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- W8376504 abstract "because of field experience and compatibility with the bill of material PW2037 design. The simulated flight cycle for the ground based engine tests consisted of 4.5 min idle, 1.5 min takeoff and intermediate conditions in a PW2037 engine with average uncorrected combustor exit temperature of 1527 C. Post test evaluation consisting of visual observations and fluorescent penetrant inspections was conducted after 500 cycles of testing. No loss of integrity in the burner liner was shown." @default.
- W8376504 created "2016-06-24" @default.
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- W8376504 date "1968-12-01" @default.
- W8376504 modified "2023-09-26" @default.
- W8376504 title "Evaluation of proposed test cell liner materials and a collimator design" @default.
- W8376504 doi "https://doi.org/10.2172/4270145" @default.
- W8376504 hasPublicationYear "1968" @default.
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