Air enters the compressor of a simple gas turbine at p1= 14 lbf/in.2, t1 = 520degreer, and a volumetric flow rate of 10,000 ft3 / min. the isentropic efficiencies of the compressor and turbine are 83% and 87%, respectively. the compressor pressure ratio is 14 and the temperature at the turbine inlet is 2500 r. on the basis of an air-standard (not cold air-standard) analysis, calculate the thermal efficiency of the cycle. the net power developed, in btu/h.

A3-mm-thick panel of aluminum alloy (k 177 w/m-k, c 875 j/kg-k and ? = 2770 kg/m) is finished on both sides with an epoxy coating that must be cured at or above t,-150°c for at least 5 min. the production line for the curing operation involves two steps: (1) heating in a large oven with air at ts,0-175°c and a convection coefficient of h, 40 w/m2. k, and (2) cooling in a large chamber with air at 25°c and a con- vection coefficient of he 10 w/m2.k. the heating portion of the process is conducted over a time interval te which exceeds the ime required to reach 150°c by 5 min (h = r + 300 s). the coating has an emissivity of ? = 0.8, and the temperatures of the oven and chamber walls are 175 and 25°c, respectively. if the panel is placed in the oven at an initial temperature of 25°c and removed from the chamber at a safe-to-touch tempera ture of 37°c, what is the total elapsed time for the two-step curing operation?