- #1
wisemo
- 7
- 0
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
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