Numerical Predictions of Stanton Numbers, Skin Friction Coefficients, Aerodynamic Losses, and Reynolds Analogy Behavior for a Transsonic Turbine Vane
Author:
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
http://www.tandfonline.com/doi/pdf/10.1080/10407780500324798
Reference19 articles.
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3. R. J. Boyle , B. L. Luci , V. G. Verhoff , W. P. Camperchioli , and H. La , Aerodynamics of a Transitioning Turbine Stator over a Range of Reynolds Numbers , ASME Paper 98-GT-285 , 1998 .
4. J. E. Fitzgerald , A. J. Niven , and M. R. D. Davies , Turbine Blade Aerodynamic Wall Shear Stress Measurements and Predictions , ASME Paper 98-GT-562, International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm , Sweden , 1998 .
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