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Calculate the static thrust of the engine.

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1. For the engine in Prob. 9.1, calculate the mean effective pressure. 2. Consider a turbojet mounted on a stationary test stand at sea level. The inlet and exit areas are the same, both equal to 0.45 m2. The velocity, pressure, and temperature of the exhaust gas are 400 m/s, 1.0 , and 750 K, respectively. Calculate the static thrust of the engine. Prob. 9.1 A reciprocating engine for light aircraft, modeled after the Lycoming 0-235 engine, has the following characteristics: bore = 11.1 , stroke = 9.84 , number of pistons = 4, compression ratio = 6.75, mechanical efficiency= 0.83. It is connected to a propeller with an efficiency of 0.85. If the fuel-to-air ratio is 0.06 and the pressure and temperature in the intake manifold are 1 and 285 K, respectively, calculate the power available from the engine-propeller combination at 2800 rpm.

 
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