Centrifugal force on rotating blades

AI Thread Summary
To calculate the centrifugal force on airfoil blades at constant angular speed, determine the average force along the blade and multiply it by the blade length to find the total force at the root. This can be simplified by estimating the center of mass and treating the forces as concentrated at that point, using the formula CF = Mass × Omega² × Radius. The discussion also mentions a "Maximum regulating test" for axial fans, which has a limit of +/- 15,000 kilo-pounds, though details on its execution are sought. Understanding these calculations and tests is crucial for assessing blade performance under rotational forces. The conversation highlights the importance of accurately determining forces in rotating systems.
wisemo
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Hi everyone,

I've got a set of airfoil blades here which are homogenious and have a constant profile (x-section). Each blade is of equal length (as should be).
What would the best way be to calculate the centrifugal force on the blade root as a result of constant angular speed? say o - rads/s

I've just gotten a little confused about involving the 'centre of gyration'.

thanks

mo
 
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If you can calculate the average force throughout the blade, and multiply by the length of the blade, that will give you the total force, all of which is felt at the root of the blade.
 
Easy, since blade is constant section, estimate the centre of mass position and treat the root forces/stresses as if the mass was concentrated at the mass centre - ie CF = Mass.Omega^2.Radius.
 
I have recently came across a test - "Maximum regulating test" with a limit of +/- 15000 kilo-pound been performed on axial fans. Can anyone explain me what this test is all about & how it is performed.
Thanks in advance.
 
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