A comparison of experimental and computational heat transfer results for a leading edge impingement system

Leading edge impingement systems are increasingly being used for high pressure turbine blades in gas turbine engines, in regions where very high heat loads are encountered. The flow structure in such systems can be very complex and high resolution experimental data is required for engine-realistic s...

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Những tác giả chính: Pearce, R, Ireland, P, Dane, E, Telisinghe, J
Định dạng: Journal article
Được phát hành: MDPI 2018

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