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)]

doi:10.1115/1.1285853

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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. Jul 2000, 122(3): 415 (1 pages)

https://doi.org/10.1115/1.1285853

Published Online: July 1, 2000

[S0889-504X(00)03102-0]

1.

Schreiber, H. A., Steinert, W., and Ku¨sters, 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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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)]

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