Design of highly efficient propeller blades |
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| Authors: | V G Gainutdinov N V Levshonkov |
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| Institution: | 1. Tupolev Kazan National Research Technical University, Kazan, Russia
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| Abstract: | A technique of evaluating the design parameters for a highly efficient propeller (with optimal geometrical twist) is given. The results of comparative calculations for design parameters of a high-altitude aircraft propeller are presented taking into account air density and compressibility. |
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