Though dissimilar, these two subjects have been united because they have some points in common. The computation of the movement of an airplane can only be correctly established if we are in a position to know exactly the thrust and resisting torque of the propeller for the various values of slip, which may vary greatly according to circumstance. The first part of the work concerns propellers and introduces as a fundamental variable, the true slip (delta) with respect to the effective pitch, which is the advance per revolution of the propeller corresponding to no thrust. The second part deals with characteristic curves of an airplane.
Resume of the theory of naval and aerial propulsive propellers and of airplanes in the rectilinear flight
1921-04-01
Sonstige
Keine Angabe
Englisch
Racing propellers for light airplanes
Engineering Index Backfile | 1932
|Adaptation of propellers to airplanes
Engineering Index Backfile | 1923
|Racing propellers for light airplanes
Engineering Index Backfile | 1931
|Characteristics of propellers for turboprop airplanes
Engineering Index Backfile | 1952
|Speculations on propellers for stratosphere airplanes
Engineering Index Backfile | 1937
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