

![Power output = 32 mw = 32x103 kw a power = micp (B3-T4) 32000 = mix 1.053 ( 900- 567.40] m = 91.36 kgs. mass = ကံ ၃ ပT = 91.3](http://img.homeworklib.com/questions/1cec0460-d4d8-11ea-b2a1-45306f9071b7.png?x-oss-process=image/resize,w_560)
6. Repeat Problem 5, but use constant specific heats at the average temperature of (900 K+310...
Problem 9.106 using varaiable specific heat assumption
(Non-Ideal Regenerative Brayton Cycle)
9-105 A gas turbine for an automobile is designed with a regenerator. Air enters the compressor of this engine at 100 kPa and 30°C. The compressor pressure ratio is 8; the maximum cycle temperature is 800°C; and the cold airstream leaves the regenerator 10°C cooler than the hot airstream at the inlet of the regenerator. Assuming both the compressor and the tur- bine to be isentropic, determine the rates...
Air enters the compressor of a regenerative air-standard Brayton cycle with a volumetric flow rate of 20 m3/s at 0.8 bar, 280 K. The compressor pressure ratio is 20, and the maximum cycle temperature is 1950 K. For the compressor, the isentropic efficiency is 92% and for the turbine the isentropic efficiency is 95%. For a regenerator effectiveness of 86%, determine: (a) the net power developed, in MW. (b) the rate of heat addition in the combustor, in MW. (c)...
Help Save & Exit Submit Required information A Brayton cycle with regeneration using air as the working fluid has minimum and maximum temperatures in the cycle are 310 and 1150 K. Assume an isentropic efficiency of 75 percent for the compressor and 82 percent for the turbine and an effectiveness of 68 percent for the regenerator. Use variable specific heats for air a pressure ratio of 7. The Determine the air temperature at the turbine exit. (You must provide an...
Air enters the compressor of a regenerative air-standard Brayton cycle with a volumetric flow rate of 100 m3/s at 0.8 bar, 280 K. The compressor pressure ratio is 20, and the maximum cycle temperature is 2100 K. For the compressor, the isentropic efficiency is 92% and for the turbine the isentropic efficiency is 95%. For a regenerator effectiveness of 86%, determine: (a) the net power developed, in MW. (b) the rate of heat addition in the combustor, in MW. (c)...
A combined cycle power plant has a net power output of 272 MW. Air enters the compressor of the Brayton cycle at 100 kPa and 17oC. The pressure ratio is 19, the turbine inlet temperature is 1660 K and the gases leaving the turbine are used to heat the steam of the Rankine cycle to 600oC and 5 MPa. The combustion gas leaves the heat exchanger (HRSG) at 390 K and the condenser pressure is 20 kPa. The isentropic efficiency...
Do problem 9.128E using
variable specific heat assumptions instead of constant.
Please don't use constant specific heat
assumption
Solution 9.128E Problem Statement Reconsider Prob. 9–127E. Determine the change in the rate of heat addition to the cycle when the isentropic efficiency of each compressor is 88 percent and that of each turbine is 93 percent. Problem 9.127E A gas turbine operates with a regenerator and two stages of reheating and intercooling. Air enters this engine at 14 psia and 60°F;...
3a. A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 14.7 and 200 psia. Air enters the compressor at 77°F at a rate of 28 lbm/s and leaves at 750°F. Fuel is burned in the combustion chamber and the combustion gases enter the turbine at 2000°F. Combustion gases leave the turbine whose isentropic efficiency is 85 percent. Treating the combustion gases as air and using constant specific heats evaluated at 900°F, determine (a) the...
2. Air enters the compressor of a regenerative gas turbine engine at 310 K and 100 kPa, where it is compressed to 900 kPa and 650 K. The regenerator has an effectiveness of 80%and the air enters the turbine at 1400 K. For a turbine isentropic efficiency of 90%, , then: (a) Sketch the T-s diagram of the cycle. (b) Determine the amount of heat transfer in the regenerator (c) Calculate the thermal efficiency of the cycle (d) Determine the...
3. Air is used as the working fluid in a simple ideal Brayton cycle that has a pressure ratio of 12, a compressor inlet temperature of 300 K, and a turbine inlet temperature of 1000 K. Determine the required mass flow rate of air for a net power output of 90 MW. Assume constant specific heats at room temperature.
A combined cycle gas turbine/vapor power plant uses the turbine exhaust as the energy source for the boiler. Each power system uses a single turbine. The gas power system is modeled as an ideal air-standard Brayton cycle. The vapor power system is modeled as an ideal Rankine cycle. Given specific operating conditions determine the temperature and pressure at each state, the rate of heat transfer in the boiler, the power output of each turbine, and the overall efficiency. --Given Values--...