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The conduit between the turbine and nozzle nozzle output of

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The conduit between the turbine and nozzle (nozzle) output of an engine is 0.60 m in diameter. The gas has a pressure and a temperature of stagnation of 275 KPa and 700 K, respectively. The gas mass flow is 82 kg / s. Specify the relevant areas of nozzle to expand the gas to standard atmospheric pressure. Calculate the force required to maintain the nozzle in the duct. The gas is k = 1.4 and R = 265 n.m / kg.K

Reference no: EM13636878

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