Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference26 articles.
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3. Natural transition of boundary layers – the effects of turbulence, pressure gradient and flow history;Abu-Ghannam;J. Mech. Eng. Sci.,1980
4. Investigations of boundary layer transition in an adverse pressure gradient;Gostelow;ASME J. Turbomachinery,1989
5. K. Dullenkopf, R.E. Mayle, ASME Paper No. 94-GT-174, 1994
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