Cooling methods for gas turbine blade leading edge: Comparative study on impingement cooling, vortex cooling and double vortex cooling
Author:
Publisher
Elsevier BV
Subject
Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics
Reference25 articles.
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4. Heat Transfer Performance of Internal Cooling Channel with Single-Row Jet Impingement Array by Varying Flow Rates;Siw,2017
5. S. Computational flow and heat transfer of a row of circular jets impinging on a concave surface;Kumar;Heat Mass Transf.,2008
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