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...
Главные авторы: | Pearce, R, Ireland, P, Dane, E, Telisinghe, J |
---|---|
Формат: | Journal article |
Опубликовано: |
MDPI
2018
|
Схожие документы
-
A Comparison of Experimental and Computational Heat Transfer Results for a Leading Edge Impingement System
по: Robert Pearce, и др.
Опубликовано: (2018-11-01) -
Sweeping jet impingement heat transfer on a simulated turbine vane leading edge
по: Mohammad A. Hossain, и др.
Опубликовано: (2018-09-01) -
Numerical investigation on heat transfer in an advanced new leading edge impingement cooling configuration
по: G. Lin, и др.
Опубликовано: (2015-12-01) -
Comparison of full surface local heat transfer coefficient and flow field studies beneath sharp-edged and radiused entry impinging jets
по: Gillespie, D, и др.
Опубликовано: (1996) -
Conjugate Heat Transfer Study of Combined Impingement and Showerhead Film Cooling Near NGV Leading Edge
по: Dileep Chandran, и др.
Опубликовано: (2015-01-01)