A simplified procedure has been developed to calculate the l-P oscillating aerodynamic thrust loads on single-rotation propellers in pitch at zero yaw on tractor airplanes. The application of this procedure requires only a knowledge of the upflow angles at the horizontal center line of the propeller disk.
Calculation of the 1.P Oscillating Aerodynamic Loads on Single- Rotation Propellers in Pitch on Tractor Airplanes
1955
29 pages
Report
Keine Angabe
Englisch
Engineering Index Backfile | 1955
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