Advanced Nonaxisymmetric Endwall Contouring for Axial Compressors by Generating an Aerodynamic Separator-Part II: Experimental and Numerical Cascade Investigation
Journal of turbomachinery ; 133 , 2 ; 21027-21028
2011
Article (Journal)
English
Heat Transfer for a Turbine Blade With Nonaxisymmetric Endwall Contouring
Online Contents | 2011
|British Library Conference Proceedings | 1999
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