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- W182986236 abstract "The results of low cycle fatigue testing on turbine blades for use in hydrogen/oxygen rocket engines is presented. Cored blade and cored blades with circulation were tested in the MSFC thermal fatigue tester. Both blade configurations showed significant low cycle fatigue life improvements when compared to baseline solid blades." @default.
- W182986236 created "2016-06-24" @default.
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- W182986236 date "1985-09-01" @default.
- W182986236 modified "2023-09-27" @default.
- W182986236 title "Turbine blade thermal fatigue testing Pratt and Whitney aircraft hollow core blades" @default.
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