bennygod
Structural
- Dec 5, 2005
- 6
Hi all, long time listener, first time poster. It's been a while since my uni days of performign heat transfer calculations, so any guidance with a suitable method for the follwoing problem would be appreciated.
I have a solid rotor wrapped in a carbon sleeve. I know the k for both stator and sleeve (21 and 0.6 W/m.K). I also know the Q dumped from rotor into carbon = 500 W. The outside dia. of the sleeve is air cooled by air at 40C and ~70 m/s. Given that the air flow is turbulent and the Re (100000), Nu (200) and Pr are known, as is h (~200 W/m2.K).
I've got lots of info on composite hollow pipes where hot air/gas moves through the centre of the pipe and heat transfer takes place between pipe wall and then some extra lagging/insulation, but not sure how well this would translate for my needs?
My questions are:
Q1. How to calculate heat removed by air.
Q2. If the rotor was required to be kept at a certain temperature, can the air speed be determined?
Any help will be greatly received.
Cheers.
I have a solid rotor wrapped in a carbon sleeve. I know the k for both stator and sleeve (21 and 0.6 W/m.K). I also know the Q dumped from rotor into carbon = 500 W. The outside dia. of the sleeve is air cooled by air at 40C and ~70 m/s. Given that the air flow is turbulent and the Re (100000), Nu (200) and Pr are known, as is h (~200 W/m2.K).
I've got lots of info on composite hollow pipes where hot air/gas moves through the centre of the pipe and heat transfer takes place between pipe wall and then some extra lagging/insulation, but not sure how well this would translate for my needs?
My questions are:
Q1. How to calculate heat removed by air.
Q2. If the rotor was required to be kept at a certain temperature, can the air speed be determined?
Any help will be greatly received.
Cheers.