The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.
Aerodynamic Design of Supersonic Propellers From Structural Considerations
1952
23 pages
Report
No indication
English
Aerodynamic design of supersonic propellers from structural considerations
Engineering Index Backfile | 1952
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