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