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- W2088398908 abstract "A three-dimensional finite element elastoplastic strain analysis was performed for the throat section of regeneratively cooled rocket engine combustion chamber. The analysis included thermal and pressure loads, and the effects of temperature dependent material properties, to determine the strain range corresponding to the engine operating cycle. The strain range was used in conjunction with OFHC copper isothermal fatigue test data to predict engine low-cycle fatigue life. The analysis was performed for chamber configuration and operating conditions corresponding to a hydrogen-oxygen chamber which was fatigue tested to failure at the NASA Lewis Research Center." @default.
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- W2088398908 date "1974-08-16" @default.
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- W2088398908 title "Low-cycle fatigue analysis of a cooled copper combustion chamber" @default.
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- W2088398908 doi "https://doi.org/10.2514/6.1974-1079" @default.
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