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- W2077762217 abstract "This paper reviews the methods for predicting boundary-layer behavior on flat and curved surfaces under conditions experienced in gas turbine engines and the resultant heat transfer to the turbine rotor blades. Particular attention is given to the effects of streamwise pressure gradient and the intensity of mainstream turbulence on transition phenomena. The time-mean heat transfer across a boundary-layer under unidirectional oscillatory mainstream flow, such as might be initiated in a combustion chamber, is considered. The relevance of flat plate predictions and correlations to rotating turbine blades is also discussed." @default.
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- W2077762217 date "1974-03-30" @default.
- W2077762217 modified "2023-09-23" @default.
- W2077762217 title "A Review of the Bases of Predicting Heat Transfer to Gas Turbine Rotor Blades" @default.
- W2077762217 doi "https://doi.org/10.1115/74-gt-27" @default.
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