Investigation of blade-row flow distributions in axial-flow-compressor stage consisting of guide and rotor-blade row
1950
54 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Axial Compressor and Turbine Stage Design Using Through-Flow and Blade-To-Blade Codes
British Library Conference Proceedings | 1999
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