Visualization and quantitation of unsteadiness of film cooling near stagnation line of a double-wall cooled vane leading edge
Author:
Funder
china aerospace science and technology corporation
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s12650-022-00870-7.pdf
Reference27 articles.
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3. Bunker RS (2013) Gas turbine cooling: moving from macro to micro cooling. In: proceedings of ASME turbo expo, GT2013-94277
4. Fawcett RJ, Wheeler APS, He L, Taylor R (2012) Experimental investigation into unsteady effects on film cooling. ASME J Turbomach 134:021015
5. Freund O, Rehder HJ, Schaefer P, Roehle I, (2011) Experimental investigations on cooling air ejection at a straight turbine cascade using PIV and QLS. In: proceedings of ASME turbo expo, GT2011-45296
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