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[ASME ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition - The Hague, Netherlands (Monday 13 June 1994)] Volume 1: Turbomachinery - Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part II — A Model for Supersonic Flow
König, W. M., Hennecke, D. K., Fottner, L.Year:
1994
Language:
english
DOI:
10.1115/94-gt-336
File:
PDF, 649 KB
english, 1994