Operating conditions of conventional airfoil type propeller or helicopter rotor in both subsonic and supersonic regions are separately considered, in absence of direct shock and blade interference effects and other disturbances; performance is approximately predicted by applying conventional strip-type analysis and results of 2-dimensional airfoil theory.
Effectiveness of propellers at high speeds
Aircraft Eng
Aircraft Engineering ; 31 , n 370
1959
5 pages
Aufsatz (Zeitschrift)
Englisch
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Effectiveness of Propellers at High Speeds
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