he air passage for cooling a gas turbine vane can
Chapter 8, Problem 8.50(choose chapter or problem)
he air passage for cooling a gas turbine vane can beapproximated as a tube of 3-mm diameter and 75-mmlength. The operating temperature of the vane is 650C,and air enters the tube at 427C.(a) For an airflow rate of 0.18 kg/h, calculate the airoutlet temperature and the heat removed from thevane.(b) Generate a plot of the air outlet temperature as afunction of flow rate for 0.1??0.6 kg/h. Com-pare this result with those for vanes having 2- and4-mm-diameter tubes, with all other conditionsremaining the same
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