Flow visualization of longitudinal vortices induced by an inclined impinging jet in a crossflow--effective cooling of high temperature gas turbine blades

By Nakabe K.   Inaoka K.   Ai T.   Suzuki K.  

Energy Conversion and Management, Vol. 38, Iss. 10, 1997-09 ,pp. : 1145-1153

Elsevier

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Effect of coolant injection angle and cooling hole dimensions on transpiration cooled gas turbine cycle performance

By Kumar S   Singh O  

Journal of the Energy Institute, Vol. 86, Iss. 3, 2013-08 ,pp. : 140-146

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Turbulence intensity effects on film cooling and heat transfer from compound angle holes with particular application to gas turbine blades

By Al-Hamadi A.K.   Jubran B.A.   Theodoridis G.  

Energy Conversion and Management, Vol. 39, Iss. 14, 1998-09 ,pp. : 1449-1457

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Linear Stability Prediction of Vortex Structures on High Pressure Turbine Blades †

By Zauner Markus   Sandham Neil D.   Wheeler Andrew P. S.   Sandberg Richard D.  

International Journal of Turbomachinery, Propulsion and Power, Vol. 2, Iss. 2, 2017-05 ,pp. : 8-8

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Integration of steam injection and inlet air cooling for a gas turbine generation system

By Wang F.J.   Chiou J.S.  

Energy Conversion and Management, Vol. 45, Iss. 1, 2004-01 ,pp. : 15-26

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