theonlydave
Mechanical
- Feb 10, 2005
- 15
I have a specific problem about the cooling rate of a blade attached to a rotor spining at 20000rpm. The blade would achieve a temperature of 1200°C after heating and I need to find the cooling rate of the blade tip and its final temperature after a single quarter revolution. Since the blade would revolve at 20000rpm, a quarter revolution would take only 7.5 e-4 seconds. The blade tip speed would be 379.7 m/s. The radius of the rotor is 175mm and the blade dimension is 15mm X 1.5mm with a height of 6.3mm in the direction of the rotor radius. There are 24 blades on the rotor so there will be 15° offset angle between the rotors at the rotor centre. I done a theoretical modeling of the problem, predicting turbulent wake at the blade tip. Does anyone have any idea how to compute the convective heat transfer coefficient? Can I use the equation for a transient heat conduction of a semi infinite body with a surface convection boundary here?
Dave
Dave