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- W1640285426 abstract "Material thermal conductivity was analyzed for its effect on the thermal performance of air cooled gas turbine components, both with and without a ceramic thermal-barrier material, tested at reduced temperatures and pressures. The analysis shows that neglecting the material thermal conductivity can contribute significant errors when metal-wall-temperature test data taken on a turbine vane are extrapolated to engine conditions. This error in metal temperature for an uncoated vane is of opposite sign from that for a ceramic-coated vane. A correction technique is developed for both ceramic-coated and uncoated components." @default.
- W1640285426 created "2016-06-24" @default.
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- W1640285426 date "1980-05-01" @default.
- W1640285426 modified "2023-09-24" @default.
- W1640285426 title "Extension of Similarity Test Procedures to Cooled Engine Components With Insulating Ceramic Coatings" @default.
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