Correction factors for ideal angle of attack and camber due to loading are presented for 3 Bladed 0.2R hub propellers.
The factors are based on propeller lifting surface theory. Correction factors for ideal angle of attack due to thickness are not included. The propellers are optimum free-running propellers with chordwise loadings identical to NACA a = 0.8 meanline.
Lifting surface corrections for 3 bladed optimum propellers
International Shipbuilding Progress ; 18 , 208 ; 437-452
1971-12-01
16 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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