Influence of aircraft and installation characteristics on design of propellers in 500 to 1000 shp class is shown; these characteristics have significant effect on propeller performance, weight, and stress levels; effects of aircraft geometry and flight conditions on propeller blade selection and pitch change system design are considered; selection of propeller blade is based on desired propeller performance, propeller diameter limitation, and steady and vibratory stress levels; magnitude of steady stress depends upon power loading of blade; magnitude of vibratory stress depends upon nacelle tilt, gross weight, lift characteristics and other aircraft parameters; examples of installations.
Propeller design consideration for turbine powered aircraft
SAE -- Paper
SAE Meeting ; 1968 Propellers
1968
10 pages
Aufsatz (Konferenz)
Englisch
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