A Small Perturbation Theory for Cycloidal Propellers

Citation

James, Edwin Charles (1971) A Small Perturbation Theory for Cycloidal Propellers. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/Z979-K031. https://resolver.caltech.edu/CaltechTHESIS:03242015-131614633

Abstract

A hydromechanical theory is developed for cycloidal propellers for two limiting modes of operation wherein U » ΩR and U « ΩR, with U the rectilinear propeller speed (speed of advance) and ΩR the rotational blade speed. A first order theory is developed from the basic principles of the kinematics and dynamics of fluid motion and proceeds from the point of view of unsteady hydrofoil theory.

Explicit expressions for the instantaneous forces and moments produced by blade motions are presented. On the basis of these results an optimization procedure is carried out which minimizes the energy loss under the constraint of specified mean thrust. Under optimal conditions the propeller is found to possess high Froude efficiencies in both the high and low speed modes of propulsion. This efficiency is defined as the ratio of the average useful work obtained during one cycle of propeller operation to the average power input required to sustain the motion of the propeller during the cycle.

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