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1) Steam at 200 psia and 600 F is supplied to a turbine and exhausted at...
ANSWER PLEASE PROBLEM #2 (68 pts.) Steam at 200 psia, 600°F (State 1) enters an adiabatic...
ANSWER PLEASE
PROBLEM #2 (68 pts.) Steam at 200 psia, 600°F (State 1) enters an adiabatic turbine cperating at steady state with a mass flow rate of 16.5 lbm/min and exits at 15 psia, 240°F (State 2), Neglecting the changes in kinetic and potential energies and assuming the surroundings to be at T.- 537 R. Determine: a) the actual power output, in Btu/min. b) the reversible (or maximum) power output, in Btu/min. c) the rate of exergy destruction, in Btu/min....
Air initially at 120 psia and 500*F is expanded by an adiabatic turbine to 15 psia...
Air initially at 120 psia and 500*F is expanded by an adiabatic turbine to 15 psia and 200* F. Assuming air can be treated as an ideal gas and has variable specific heat. a) Determine the specific work output of the actual turbine (Btu/lbm). b) Determine the amount of specific entropy generation during the irreversible process (Btu/lbm R). c) Determine the isentropic efficiency of this turbine (%). d) Suppose the turbine now operates as an ideal compressor (reversible and adiabatic)...
steam enters a turbine at 1000 psia and 1000 degrees celsius, and leaves at 5Psia and...
steam enters a turbine at 1000 psia and 1000 degrees celsius,
and leaves at 5Psia and 97% quality, the turbine is adiabatic and
the power output is 25000 hp.
Calculate:
1- the work of the turbine ( in btv/lbm)
2- the mass flow rate in lbm/s, if the work of the turbine is
353.399 btv/lbm
3- the inlet diameter, if the mass flow rate is 60 lbm/s
NOTE: inlet velocity ≈ exit velocity =80 ft/s
1hp=2545 btv/hr
- Steam turbine...
Problem 4 A steam turbine is used to generate power. The turbine expansion process is "adiabatic,"...
Problem 4 A steam turbine is used to generate power. The turbine expansion process is "adiabatic," this means that there is no heat transfer during this process. The inlet and exit conditions are listed below T1 = 600-degF P2 10-psia T2 1932-degF x2 0.9 P1 500-psia BTU lb Adiabatio Steam Turbine h1:= 1299.1·ww s1 1.5652. BTU b-R Qloss 0 BTU lb At 10 psia, BTU h,-1143.3- BTU BTU lb s,-1.788-en lb-R hr:= 161.2- S(30-2836. A. Determine the work of the...
Problem 1 - Gas Turbine Engine. Assume the gas turbine engine operates on basic non-ideal Brayton...
Problem 1 - Gas Turbine Engine. Assume the gas turbine engine operates on basic non-ideal Brayton cycle with the following specifications Inlet Condition: Dry air at 537 R and 14.7 psia Pressure Ratio: 24.2 Actual Exhaust Temperature: 950 F Compressor and Turbine Efficiency: 85% Actual Power Output 34 MW Using given/assumed values, determine: a) firing temperature, b) cycle efficiency, c) air mass flow rate. Problem 2- HRSG. Assume the HRSG is used to produce saturated steam at 600 psia using...
Steam with the mass flow rate of 0.75 kg/s enters an adiabatic turbine steadily at 19 MPa, 600°C and 150 m/s
Steam with the mass flow rate of 0.75 kg/s enters an adiabatic turbine steadily at 19 MPa, 600°C and 150 m/s, and leaves at 150 kPa and 350 m/s. The isentropic efficiency of the turbine is 85%. Neglect potential energy. (I) Determine the exit temperature of the steam, and its quality (if saturated mixture) (ii) Calculate the actual power output of the turbine, in kW (iii) Illustrate a T-s diagram with respect to saturation lines for the isentropic process by clearly indicating all pressure, temperature,...
1. A combined gas-steam power cycle uses a single gas turbine cycle for the air cycle...
1. A combined gas-steam power cycle uses a single gas turbine
cycle for the air cycle and a simple Rankine cycle for the water
vapor cycle. Atmospheric air enters the compressor at a rate of
88.2 lbm / s, at 14.7 psia and 59 ° F, and the maximum gas cycle
temperature is 1,742 ° F. The pressure ratio in the compressor is
7. The isentropic efficiency of both the compressor and the turbine
is 80%. Gas exits the heat...
A steam plant generates saturated steam at 600 psia. The condensate exits the condenser at 5...
A steam plant generates saturated steam at 600 psia. The condensate exits the condenser at 5 psia and 158 ºF. The feed pump and main turbine are isentropic. Find: a. Is the condensate sub-cooled? If so, how much condensate depression is there (ºF) b. Is the generated steam superheated? If so, how much superheat is there (ºF)? c. Determine all four state point enthalpy (h) values (BTU/lbm).
10. (25 Points) Steam enters an insulated nozzle at 140 psia, 600 F with a velocity...
10. (25 Points) Steam enters an insulated nozzle at 140 psia, 600 F with a velocity of 100 ft/s. It leaves the nozzle at 20 psia, 360°F. The mass flow rate is 10 lbm/s. Find: Ans a) b) Ans. The actual kinetic energy of the steam at the exit, in Btu The exit velocity in ft/s for part a) The exit cross sectional area of the nozzle, in in The nozzle isentropic efficiency (%) Show the actual and the ideal...
(30 pts.) 3) Steam enters an adiabatic turbine at 1400 psia and 1000 F at a...
(30 pts.) 3) Steam enters an adiabatic turbine at 1400 psia and 1000 F at a flow rate of 31.5 cfm. It exits at a quality of 90% and a pressure of 1 psia. Neglect kinetic and potential energy effects. a) Determine the power produced [hp] b) Draw P-v and T-v state diagrams showing the states and process.
ANSWER PLEASE
PROBLEM #2 (68 pts.) Steam at 200 psia, 600°F (State 1) enters an adiabatic turbine cperating at steady state with a mass flow rate of 16.5 lbm/min and exits at 15 psia, 240°F (State 2), Neglecting the changes in kinetic and potential energies and assuming the surroundings to be at T.- 537 R. Determine: a) the actual power output, in Btu/min. b) the reversible (or maximum) power output, in Btu/min. c) the rate of exergy destruction, in Btu/min....
steam enters a turbine at 1000 psia and 1000 degrees celsius,
and leaves at 5Psia and 97% quality, the turbine is adiabatic and
the power output is 25000 hp.
Calculate:
1- the work of the turbine ( in btv/lbm)
2- the mass flow rate in lbm/s, if the work of the turbine is
353.399 btv/lbm
3- the inlet diameter, if the mass flow rate is 60 lbm/s
NOTE: inlet velocity ≈ exit velocity =80 ft/s
1hp=2545 btv/hr
- Steam turbine...
Problem 4 A steam turbine is used to generate power. The turbine expansion process is "adiabatic," this means that there is no heat transfer during this process. The inlet and exit conditions are listed below T1 = 600-degF P2 10-psia T2 1932-degF x2 0.9 P1 500-psia BTU lb Adiabatio Steam Turbine h1:= 1299.1·ww s1 1.5652. BTU b-R Qloss 0 BTU lb At 10 psia, BTU h,-1143.3- BTU BTU lb s,-1.788-en lb-R hr:= 161.2- S(30-2836. A. Determine the work of the...
Problem 1 - Gas Turbine Engine. Assume the gas turbine engine operates on basic non-ideal Brayton cycle with the following specifications Inlet Condition: Dry air at 537 R and 14.7 psia Pressure Ratio: 24.2 Actual Exhaust Temperature: 950 F Compressor and Turbine Efficiency: 85% Actual Power Output 34 MW Using given/assumed values, determine: a) firing temperature, b) cycle efficiency, c) air mass flow rate. Problem 2- HRSG. Assume the HRSG is used to produce saturated steam at 600 psia using...
1. A combined gas-steam power cycle uses a single gas turbine
cycle for the air cycle and a simple Rankine cycle for the water
vapor cycle. Atmospheric air enters the compressor at a rate of
88.2 lbm / s, at 14.7 psia and 59 ° F, and the maximum gas cycle
temperature is 1,742 ° F. The pressure ratio in the compressor is
7. The isentropic efficiency of both the compressor and the turbine
is 80%. Gas exits the heat...
10. (25 Points) Steam enters an insulated nozzle at 140 psia, 600 F with a velocity of 100 ft/s. It leaves the nozzle at 20 psia, 360°F. The mass flow rate is 10 lbm/s. Find: Ans a) b) Ans. The actual kinetic energy of the steam at the exit, in Btu The exit velocity in ft/s for part a) The exit cross sectional area of the nozzle, in in The nozzle isentropic efficiency (%) Show the actual and the ideal...
(30 pts.) 3) Steam enters an adiabatic turbine at 1400 psia and 1000 F at a flow rate of 31.5 cfm. It exits at a quality of 90% and a pressure of 1 psia. Neglect kinetic and potential energy effects. a) Determine the power produced [hp] b) Draw P-v and T-v state diagrams showing the states and process.
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