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