Correction factors for camber, ideal angle due to loading, and ideal angle due to thickness based on propeller lifting surface theory for series of optimum free-running propellers with chordwise loadings same as NACA mean line and with NACA-66 chordwise thickness distributions; results show that three-dimensional camber and ideal angle are generally greater than two-dimensional camber and ideal angle at same lift coefficient. (35277)
Propeller lifting-surface corrections
Soc Nav Architects Mar Engrs -- Paper
Society of the Naval Architects and Marine Engineers -- Meeting ; 1968 Propellers
1968
29 pages
Conference paper
English
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Propeller lifting-surface corrections
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