Closure to “Discussion of ‘Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines—Part II: Experimental and Theoretical Analysis’ ” [ASME J. Turbomach., 122, No. 3, pp. 406–414 (2000)]

J. Turbomach 122(3), 415 (Jul 01, 2000) (1 page) doi:10.1115/1.1285853 History:
Copyright © 2000 by ASME
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Schreiber, H. A., Steinert, W., and Küsters, B., 2000, “Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade,” ASME Paper No. 2000-GT-263.




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