Propeller Blade Stress Estimates Using Lifting Line Theory
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Propeller Blade Stress Estimates Using Lifting Line Theory
Author | : Brenden P. Epps |
Publisher | : |
Total Pages | : 4 |
Release | : 2010 |
Genre | : Propellers |
ISBN | : |
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OPENPROP, an open-source computational tool for the design and analysis of propellers and horizontal-axis turbines, is extended to provide estimates of normal stresses in the blades for both on- and off-design operating conditions. The numerical model is based on propeller lifting theory, and the present implementation of the code includes an analysis capability to estimate the off-design performance of the propeller or turbine and to make blade stress predictions. As an example, we present the design and performance of a two-bladed propeller. Experimental measurements of the propeller performance over a wide range of off-design operating conditions agree with performance predictions. Estimates of the blade stress are given for on-design and off design operating states of the propeller.
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