arto
Mechanical
- Jun 19, 2002
- 712
I'm trying to do rotating cylinder-in-a-cylinder heat transfer design & am finding generally two different definitions for Taylor Number.
One is basically porportional to Reynold No., & the other to Reynolds Number ^squared.
The GE heat transfer book, et al, use:
Ta = [omega*radius*gap/kin.viscosity] * sqrt [gap/radius]
~Re*sqrt(gap/radius)
whereas others {i.e., Becker& Kaye, ASME Jnl H.T. may '62, et al.] use
Ta = [omega^2 * radius * gap^3]/kin.viscosity^2
~Re^2
where omega = rad/sec
These are then used to find the Nusselt No. & thence "h."
Can anybody shed some light/wisdom on this?? [The more I look [articles, internet], the more I find of either one or the other.]
Thanks
Arto
One is basically porportional to Reynold No., & the other to Reynolds Number ^squared.
The GE heat transfer book, et al, use:
Ta = [omega*radius*gap/kin.viscosity] * sqrt [gap/radius]
~Re*sqrt(gap/radius)
whereas others {i.e., Becker& Kaye, ASME Jnl H.T. may '62, et al.] use
Ta = [omega^2 * radius * gap^3]/kin.viscosity^2
~Re^2
where omega = rad/sec
These are then used to find the Nusselt No. & thence "h."
Can anybody shed some light/wisdom on this?? [The more I look [articles, internet], the more I find of either one or the other.]
Thanks
Arto