Consequences of dimensional deviations of actual blades from those of assumed standard are examined, and apparatus devised to minimize or eliminate most undesirable of them, namely, tendency to induce vibration in aircraft, is described.
Aerodynamic balancing of propellers
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 53 , n 468
1949
14 pages
Aufsatz (Zeitschrift)
Englisch
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