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.
Design of highly efficient propeller blades
Russian Aeronautics (Iz VUZ) ; 56 , 2 ; 111-116
01.04.2013
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch