Maurice Tutor

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    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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    Oct-2001 - Nov-2016

Category > Computer Science Posted 24 Sep 2017 My Price 5.00

cross-sectional area

A turbine blade 5 cm long with a cross-sectional area A = 4.5 cm2 and a perimeter P = 12 cm is made of a high alloy steel (k = 25 W/m K). The temperature of the blade attachment point is 500°C, and the blade is exposed to combustion gases at 900°C. The heat transfer coefficient between the blade surface and the combustion gases is 500 W/m2 K. Using the nodal network shown in the accompanying sketch, (a) determine the temperature distribution in the blade, the rate of heat transfer to the blade, and the fin efficiency of the blade and, (b) compare the fin efficiency calculated numerically with that calculated by the exact method.

 

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Maurice Tutor
(5)
Status NEW Posted 24 Sep 2017 12:09 PM My Price 5.00

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