The world’s Largest Sharp Brain Virtual Experts Marketplace Just a click Away
Levels Tought:
Elementary,Middle School,High School,College,University,PHD
| Teaching Since: | May 2017 |
| Last Sign in: | 407 Weeks Ago, 6 Days Ago |
| Questions Answered: | 66690 |
| Tutorials Posted: | 66688 |
MCS,PHD
Argosy University/ Phoniex University/
Nov-2005 - Oct-2011
Professor
Phoniex University
Oct-2001 - Nov-2016
EXAMPLE 6.5
Â
Experimental tests using air as the working fluid are conducted on a portion of the turbine blade shown in the sketch. The heat flux to the blade at a particular point (x*) on the surface is measured to be q"= 95,000 W/m2. To maintain a steady-state surface temperature of 800°C, heat transferred to the blade is removed by circulating a coolant inside the blade.
Â
Â
Â
q"(x*) = 95,000 W/m2
Â
Ts = 800°C
Coolant channel
Â
V = 160 m/s
T¥ = 1150°C
Â
![]()
Â
![]()
L = 40 mm
Â
Original conditions
1.   Determine the heat flux to the blade at x* if its temperature is reduced to Ts,1 = 700°C by increasing the coolant flow.
2.   Determine the heat flux at the same dimensionless location x* for a similar turbine blade having a chord length of L = 80 mm, when the blade operates in an airflow at Too = 1150°C and V = 80 m/s, with Ts = 800°C.
Â
Â
Â
Hel-----------lo -----------Sir-----------/Ma-----------dam-----------Tha-----------nk -----------You----------- fo-----------r u-----------sin-----------g o-----------ur -----------web-----------sit-----------e a-----------nd -----------acq-----------uis-----------iti-----------on -----------of -----------my -----------pos-----------ted----------- so-----------lut-----------ion-----------.Pl-----------eas-----------e p-----------ing----------- me----------- on-----------cha-----------t I----------- am----------- on-----------lin-----------e o-----------r i-----------nbo-----------x m-----------e a----------- me-----------ssa-----------ge -----------I w-----------ill----------- be-----------