WebThe power output of the turbine is 10.2 MW.Determine (a) the temperature of the water as it leaves the turbine, (b) the quality x of the water as it leaves the turbine, (c) the inlet and outlet cross-sectional area. arrow_forward Hot combustion gases enter the nozzle of a turbojet engine at 230 kPa, 627°C, and 60 m/s and exit at 70 kPa and 450°C. WebApr 25, 2013 · 69. Gas Dynamics and Jet Propulsion – Unit 4 Problem: A turbo jet propels an aircraft at a speed of 900 kmph while taking 3000 kg of air per minute. The isentropic enthalpy drop in the nozzle is 200 kJ/kg and nozzle efficiency is 90%. The air fuel ratio is 85 and the combustion efficiency is 95%.

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WebAir - Thermophysical Properties - Thermal properties of air at different temperatures - density, viscosity, critical temperature and pressure, triple point, enthalpi and entropi, … WebIt is defined as the product of the specific heat capacity of air at constant pressure and dry bulb temperature h = c p (T) C p: Specific heat of air at constant pressure C p (AIR) : 1.005 kJ/kg-K T: Dry Bulb Temperature Specific Enthalpy of ethanol The specific enthalpy of ethanol (C 2 H 5 OH) is 2.46 J/g℃ property inveraray

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