Q1: Steam enters a nozzle at 15 m/sec at 0.6 mPa and 700oC and leaves at 0.2 mPa at 400oC,the velocity (m/sec) at the exit is most nearly (assume no heat loss). NOTE: 1 kJ/kg = 1000 m2 /s
Q2: How much work (kJ) is done by an engine which contains 1 kg of water that goes from 0.6MPa, 900oC to 0.10 MPa, 150oC if 1,000 kJ of heat is added?
Please solve both questions. Thank you
Q1: Steam enters a nozzle at 15 m/sec at 0.6 mPa and 700oC and leaves at...
Steam enters a nozzle operating at steady state at 30 bar, 320 deg C with a velocity of 100 m/sec. The exit pressure and temperature are 10 bar and 200 deg C respectively. The mass rate of flow of steam is 2 kg/sec. Neglect heat transfer and potential energy. Determine, exit velocity in m/sec and inlet and exit flow areas in m2.
1. Water enters the constant 130-mm inside-diameter tubes of a boiler at 7 MPa and 65°C and leaves the tubes at 6 MPa and 450°C with a velocity of 80 m/s. Calculate the velocity of the water at the tube inlet and the inlet volume flow rate. [5-14] 2. Air enters a nozzle steadily at 50 psia, 140°F, and 150 ft/s and leaves at 14.7 psia and 900 ft/s. The heat loss from the nozzle is estimated to be 6.5...
5-30 Air enters an adiabatic nozzle steadily at 300 kPa, 200°C, and 30 m/s and leaves at 100 kPa and 180 m/s. The inlet area of the nozzle is 80 cm². Determine (a) the mass flow rate through the nozzle, (b) the exit temperature of the air, and (c) the exit area of the nozzle. Answers: (a) 0.5304 kg/s, (b) 184.6°C, (c) 38.7 cm P = 300 kPa T, = 200°C Vi = 30 m/s A = 80 cm AIR...
Hot air at 1.0 MPa and 600 °C enters to a circular cross section nozzle and is expanded to 0.6 MPa isentropically. For a throat diameter of 10 mm, find: a. The type of nozzle required b. The velocity of flow at the exit c. Temperature of flow at the exit d. Velocity of flow at the throat e. Mass flow rate through the nozzle Assume k 1.40, cp 1.004 kJ/kgK, cv 0.717 kJ/kgK, R-287 J/kgK for air Hot air...
2 5: Steam enters an adiabatic diffuser at 0.3 MPa, 200 °C, 440 m/s and leaves at 0.5 MPa, 250 C through an 800 cm2 opening. Determine the exit velocity, m/s, and the mass flowrate, kg/s.
Problem 4 Steam enters a nozzle at 500°C and 500 kPa with a velocity of 15 m/s; it exits the nozzle at 200°C and 100 kPa while losing heat at a rate of 30 kW. Given that the mass flow rate of the steam is 1.688 kg/s, determine the velocity of the steam at the nozzle exit.
3. Steam enters a nozzle at 400°C and 800 kPa with a velocity of 5 m/s and leaves at 500 kPa and 350°C, while losing 60 kJ/kg of heat. For an inlet area of 0.5 m², determine the velocity. volumetric flow rate and mass flow rate at the outlet
Steam enters an adiabatic nozzle at 400 °C and 800 kPa with a velocity of 16 m/s. It leaves the nozzle at 300 °C and 400 kPa. The inlet area of the nozzle is 800 cm2. Determine; a. The mass flow rate through the nozzle, in kg/s Ans. _kg/s b. The volume flow rate of the steam at the exit, in m3/s Ans._ _m3/s The velocity of the steam at the nozzle exit, in c. m/s Ans. m/s
Steam enters a turbine at 9 MPa and T1°C and leaves at 20 kPa with a quality equal to 0.60. Neglecting the changes in kinetic and potential energies, determine T1 if the mass flow rate through the turbine is 4 kg/s. The turbine’s power output is 7.5 MW and the heat loss from the turbine is 5 kJ/kg.
2.Air enters an adiabatic nozzle in steady flow at 300 kPa, 200 C and 45 m/sec, and leaves at 100 kPa and 180 m/sec. The inlet area of the nozzle is 110 cm 2. Determine: (a) the mass flow rate through the nozzle, and mdot = _ kg/sec (b) the exit temperature T2 = OC