Question

Use cold-air-standard analysis with the fluid modeled as an ideal gas with R=0.287 kJ/kg-K and constant...

Use cold-air-standard analysis with the fluid modeled as an ideal gas with R=0.287 kJ/kg-K and constant k=1.4. Neglect changes in kinetic and potential energy. Consider a SSSF of air at 300 K and 100 kPa entering the compressor of a Simple Brayton Cycle Gas Turbine powerplant. The cycle pressure ratio is 40 and maximum cycle temperature is 1800 K. For compressor isentropic efficiency of 82% the compressor work input per unit mass = __ kJ/kg (enter the nearest positive integer value)

Homework Answers

Answer #1

note: by mistake, I have not put a negative sign before 1500, so please you can put negative sigh before 1500. then the solution becomes finally positive in results.

I hope you can understand the solution.

Thank you!!!

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
Consider a cold air-standard Diesel cycle. At the beginning of compression, 102 kPa, and 300 K....
Consider a cold air-standard Diesel cycle. At the beginning of compression, 102 kPa, and 300 K. The mass of air is 0.120 kg, the compression ratio is 16, and the cut-off ratio is 2.0 For a cold air-standard analysis use the following values: cp = 1.005 kJ/kgK, cv = 0.718 kJ/kgK, k=1.40, M=28.97 kg/kmol. Determine the following : (a) pressure at end of compression stroke, in kPa (b) temperature at end of compression stroke, in K (c) maximum temperature in...
A simple gas turbine plant working on the ideal constant pressure cycle. Air is taken into...
A simple gas turbine plant working on the ideal constant pressure cycle. Air is taken into the compressor at 1 bar, 20.2 deg C and delivered at 7.2 bar. If the temperature at the turbine inlet is 765 deg C. Calculate the ideal thermal efficiency.
Problem 6.100 SI Carbon dioxide (CO2) at 1 bar, 300 K enters a compressor operating at...
Problem 6.100 SI Carbon dioxide (CO2) at 1 bar, 300 K enters a compressor operating at steady state and is compressed adiabatically to an exit state of 10 bar, 590 K. The CO2 is modeled as an ideal gas, and kinetic and potential energy effects are negligible. For the compressor, determine: (a) the work input, in kJ per kg of CO2 flowing, (b) the rate of entropy production, in kJ/K per kg of CO2 flowing, and (c) the percent isentropic...
1) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the...
1) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the compression process, the temperature is 20°C, and the pressure is 100 kPa. The heat added is 500 kJ/kg. Determine the cycle efficiency, work output, and the heat rejected 2) An air-standard Otto cycle operates with a minimum temperature of 300 K and a maximum temperature of 1700 K. The compression ratio of the cycle is 7. At the beginning of the compression process, the...
10) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the...
10) An air-standard Otto cycle has a compression ratio of 9. At the beginning of the compression process, the temperature is 20°C, and the pressure is 100 kPa. The heat added is 500 kJ/kg. Determine the cycle efficiency, work output, and the heat rejected. 11)An air-standard Otto cycle operates with a minimum temperature of 300 K and a maximum temperature of 1700 K. The compression ratio of the cycle is 7. At the beginning of the compression process, the pressure...
2-Assuming ideal gas and constant Cp, calculate [capital delta S with hat on top] (in kJ/(kg?K))...
2-Assuming ideal gas and constant Cp, calculate [capital delta S with hat on top] (in kJ/(kg?K)) for a process where nitrogen is heated from 200 K to 800 K while changing the pressure from 2000 kPa to 1000 kPa. 1-Using the thermodynamic tables, calculate [capital delta S with hat on top] (in kJ/(kg?K)) for a process where nitrogen is heated from 200 K to 800 K while changing the pressure from 2000 kPa to 1000 kPa.
1) A nozzle is a device for increasing the velocity of a steadily flowing stream of...
1) A nozzle is a device for increasing the velocity of a steadily flowing stream of fluid. At the inlet to a certain nozzle the enthalpy of the fluid is 3025 kJ/kg and the velocity is 60 m/s. At the exit from the nozzle the enthalpy is 2790 kJ/kg. The nozzle is horizontal and there is negligible heat loss from it. (i) Find the velocity at the nozzle exit. (ii) If the inlet area is 0.1 m2 and specific volume...
Air at 1 bar, 295 K, and a mass flow rate of 0.7 kg/s enters a...
Air at 1 bar, 295 K, and a mass flow rate of 0.7 kg/s enters a compressor operating at steady state and exits at 3 bar. During the compressing from inlet to exit, the air experiences a polytropic process as PV^n=constant. m=6, n=1.48. (1) Determine the power required by the compressor. (2) Determine the heat transfer between the compressor and the surrounding. (s) Determine the rate of exergy destruction. Kinetic and potential energy effects are negligible. Let T_0 = 300...
Air at 1 bar, 295 K, and a mass flow rate of 0.7 kg/s enters a...
Air at 1 bar, 295 K, and a mass flow rate of 0.7 kg/s enters a compressor operating at steady state and exits at 3 bar. During the compressing from inlet to exit, the air experiences a polytropic process as PV^n=constant. m=6, n=1.48 (1) Determine the power required by the compressor. (2) Determine the heat transfer between the compressor and the surrounding. (s) Determine the rate of exergy destruction. Kinetic and potential energy effects are negligible. Let T_0 = 300...
A Diesel cycle engine is analyzed using the air standard method. Given the conditions at state...
A Diesel cycle engine is analyzed using the air standard method. Given the conditions at state 1, compression ratio (r), and cutoff ratio (rc) determine the efficiency and other values listed below. Note: The gas constant for air is R=0.287 kJ/kg-K. --Given Values-- T1 (K) = 322 P1 (kPa) = 120 r = 11.5 rc = 1.6 Specific internal energy (kJ/kg) at state 1: 229.86 Relative specific volume at state 1= 520.52 Relative specific volume at state 2= 45.26 Temperature...