Calculating mean radius of a gas turbine rotor (blade and hub)

AI Thread Summary
The discussion focuses on calculating the mean radius of a gas turbine rotor using the formula r_m=mdot/(2*pi*U*N). The user is struggling with unit conversions, particularly converting RPM into seconds and understanding the role of pi in the calculations. Participants suggest clarifying the calculations and emphasize the importance of accurate unit conversions. They encourage sharing full calculations for better assistance. Accurate conversions and understanding the formula are crucial for obtaining the correct mean radius.
jcm0889
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Homework Statement


I'm having difficulty obtaining an accurate value possibly due to unit conversions.


Homework Equations


r_m=mdot/(2*pi*U*N)
r_m=mean radius, ft
mdot=mass flow rate, lbm/s
U= blade velocity, ft/s
N= RPM

The Attempt at a Solution


I know that I have to convert Rpm into seconds and pi converts it 2 rads
 
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hi jcm0889! welcome to pf! :smile:

(have a pi: π and try using the X2 tag just above the Reply box :wink:)
jcm0889 said:
I know that I have to convert Rpm into seconds and pi converts it 2 rads

did you mean that?

converts R to radians :wink:

if that doesn't sort it out, show us your full calculations, and then we'll see what went wrong, and we'll know how to help! :smile:
 

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