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A simple Ideal Brayton cycle operates with air with minimum and maximum temperatures of 27C and...
A simple ideal Brayton cycle operates with air with minimum and maximum temperatures of 27°C and...
A simple ideal Brayton cycle operates with air with minimum and
maximum temperatures of 27°C and 727°C. It is designed so that the
maximum cycle pressure is 2000 kPa and the minimum cycle pressure
is 100 kPa. The isentropic efficiency of the turbine is 96 percent.
Determine the net work produced per unit mass of air each time this
cycle is executed and the cycle’s thermal efficiency. Use constant
specific heats at room temperature. The properties of air at room...
A Brayton cycle operates with air with minimum and maximum temperatures of 27 ºC and 727...
A Brayton cycle operates with air with minimum and maximum temperatures of 27 ºC and 727 ºC. It is designed so that the maximum cycle pressure is 2000 kPa and the minimum cycle temperature is 100 kPa. The isentropic efficiencies of the turbine and compressor are both 90 percent. Using constant room-temperature specific heats, (a) determine the net work produced per unit mass of air each time this cycle is executed, in kJ/kg. (b) Determine the cycle's thermal efficiency. Remember...
thermodynamic question.please just solve 9-84 9-82 A simple Brayton cycle using air as the working fluid has a pressure ratio of 10. The minimum c and maximum temperatures in the cycle are 295 an...
thermodynamic question.please just solve 9-84
9-82 A simple Brayton cycle using air as the working fluid has a pressure ratio of 10. The minimum c and maximum temperatures in the cycle are 295 and 1240 K. Assuming an isentropic efficiency of 83 percent for the com pressor and 87 percent for the turbine, determine (a) the air temperature at the turbine exit, (b) the net work output, and (c) the thermal efficiency. 9-84 Repeat Prob. 9-82 using constant specific heats...
1. A regenerative Brayton cycle operates over a pressure ratio of 8. The minimum and maximum...
1. A regenerative Brayton cycle operates over a pressure ratio of 8. The minimum and maximum temperatures in the cycle are 310 K and 1150 K, respectively. Assume an isentropic compressor efficiency of 75%, an isentropic turbine efficiency of 82%, and a regenerator effectiveness of 0.65. Using constant properties (Cp - 1.005 kJ/kgK, k = 1.4), determine: a) The T-s diagram for all processes including the isentropic processes b) The air temperature at the turbine exit c) The specific network...
An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio rp of...
An aircraft engine operates on a simple ideal Brayton cycle with
a pressure ratio rp of 9. Heat is added to the cycle at a rate of
490 kW; air passes through the engine at a rate of 1.1 kg/s; and
the air at the beginning of the compression is at P1 = 71 kPa and
T1 = 0 oC. Use constant specific heats at room temperature. The
properties of air at room temperature are cp =1.005 kJ/kg.K and k...
4. An Ideal diesel engine has a compression ratio of 20 and uses air as the...
4. An Ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200K, determine a) the thermal efficiency and b) the mean effective pressure. Assume constant specific heats for air at room temperature. 5. An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio...
9 Required information A Brayton cycle with a pressure ratio of 15 operates with air entering...
9 Required information A Brayton cycle with a pressure ratio of 15 operates with air entering the compressor at 66 kPa and O°C, and the turbine at 600℃ The properties of air at room temperature are co-1.005 kJ/kg-K and k = 1.4. Oin net CompressorT Turbine Qout Calculate the net specific work produced by this cycle treating the air as an ideal gas with constant specific heats The net specific work produced by this cycle is 165kJkg.
Need help for this Brayton Cycle problem. Please help me 4. (30 marks) A gas-turbine power plant operates on the simple...
Need help for this Brayton Cycle problem.
Please help me
4. (30 marks) A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100 kPa and 800 kPa. The T-s diagram of this cycle is shown in Fig. 2. Air enters the compressor at 30°C and leaves at 330°C at a mass flow rate of 200 kg/s. The maximum cycle temperature is 1400 K. During operation of the cycle, the net power output is measured...
An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 14.2....
An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 14.2. Heat is added to the cycle at a rate of450 kW; air passes through the engine at a rate of 1.20 kg/s; and the air at the beginning of the compression is at70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. Wnet kW Round your final answer to one decimal place....
Help Save & Exit Submit Required information A Brayton cycle with regeneration using air as the...
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...
A simple ideal Brayton cycle operates with air with minimum and
maximum temperatures of 27°C and 727°C. It is designed so that the
maximum cycle pressure is 2000 kPa and the minimum cycle pressure
is 100 kPa. The isentropic efficiency of the turbine is 96 percent.
Determine the net work produced per unit mass of air each time this
cycle is executed and the cycle’s thermal efficiency. Use constant
specific heats at room temperature. The properties of air at room...
thermodynamic question.please just solve 9-84
9-82 A simple Brayton cycle using air as the working fluid has a pressure ratio of 10. The minimum c and maximum temperatures in the cycle are 295 and 1240 K. Assuming an isentropic efficiency of 83 percent for the com pressor and 87 percent for the turbine, determine (a) the air temperature at the turbine exit, (b) the net work output, and (c) the thermal efficiency. 9-84 Repeat Prob. 9-82 using constant specific heats...
1. A regenerative Brayton cycle operates over a pressure ratio of 8. The minimum and maximum temperatures in the cycle are 310 K and 1150 K, respectively. Assume an isentropic compressor efficiency of 75%, an isentropic turbine efficiency of 82%, and a regenerator effectiveness of 0.65. Using constant properties (Cp - 1.005 kJ/kgK, k = 1.4), determine: a) The T-s diagram for all processes including the isentropic processes b) The air temperature at the turbine exit c) The specific network...
An aircraft engine operates on a simple ideal Brayton cycle with
a pressure ratio rp of 9. Heat is added to the cycle at a rate of
490 kW; air passes through the engine at a rate of 1.1 kg/s; and
the air at the beginning of the compression is at P1 = 71 kPa and
T1 = 0 oC. Use constant specific heats at room temperature. The
properties of air at room temperature are cp =1.005 kJ/kg.K and k...
4. An Ideal diesel engine has a compression ratio of 20 and uses air as the working fluid. The state of air at the beginning of the compression process is 95kPa and 20°C. If the maximum temperature in the cycle is not to exceed 2200K, determine a) the thermal efficiency and b) the mean effective pressure. Assume constant specific heats for air at room temperature. 5. An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio...
9 Required information A Brayton cycle with a pressure ratio of 15 operates with air entering the compressor at 66 kPa and O°C, and the turbine at 600℃ The properties of air at room temperature are co-1.005 kJ/kg-K and k = 1.4. Oin net CompressorT Turbine Qout Calculate the net specific work produced by this cycle treating the air as an ideal gas with constant specific heats The net specific work produced by this cycle is 165kJkg.
Need help for this Brayton Cycle problem.
Please help me
4. (30 marks) A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100 kPa and 800 kPa. The T-s diagram of this cycle is shown in Fig. 2. Air enters the compressor at 30°C and leaves at 330°C at a mass flow rate of 200 kg/s. The maximum cycle temperature is 1400 K. During operation of the cycle, the net power output is measured...
An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 14.2. Heat is added to the cycle at a rate of450 kW; air passes through the engine at a rate of 1.20 kg/s; and the air at the beginning of the compression is at70 kPa and 0°C. Determine the power produced by this engine and its thermal efficiency. Use constant specific heats at room temperature. Wnet kW Round your final answer to one decimal place....
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...
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