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The two stage compressor shown in the figure below takes in air at room condition (285...
A compressor works on a pressure of 105 kPa and temperature 300 K in a Brayton...
A compressor works on a pressure of 105 kPa and temperature 300 K in a Brayton cycle and has an efficiency of 45%. The exhaust temperature is 700 K. Find the pressure ratio and the specific heat addition by the combustion for this cycle. The inlet pressure of an air compressor is 100 kPa, with temperature 290 K, and brings it to 600 kPa, after which the air is cooled in an intercooler to 330K by heat transfer to the...
Given: Air at 20 C and 100 kPa enters the first stage, and it exits the third stage at 6400 kPa. ...
Given: Air at 20 C and 100 kPa enters the first stage, and it exits the third stage at 6400 kPa. An inter-cooler is used to cool the air between the stages back to 20°C. The compression work per unit mass of air is γ-1 where γ is the specific heat ratio, R is the gas constant, subscript "i" denotes the initial (atmospheric) conditions, and subscript "o" signifies the exiting conditions. Find: intermediate pressures so that the total work is...
Air enters a two-stage compressor at 300 K and 101 kPa. The pressure ratio of each...
Air enters a two-stage compressor at 300 K and 101 kPa. The pressure ratio of each compressor stage is 3, and there is intercooling between the stages, which reduces the temperature of the air back to 300 K. The efficiency of the compressors is 0.70; the ratio of specific heats for air, k, is 1.40; and the specific heat at constant pressure, p, is 1000 J/kg K. What would be the temperature of the air after the second compression if...
An air refrigeration plant of 70.26 kW, capacity comprises a centrifugal compressor, a cooler hea...
An air refrigeration plant of 70.26 kW, capacity comprises a centrifugal compressor, a cooler heat exchanger and an air turbine. The compressor is coupled directly to the air turbine. The compressor also receives power from another prime mover. The processes in the compressor and the turbine are adiabatic but not isentropic. Air at temperature 294 K and 85 kPa enters the compressor. It leaves the compressor at 363 K. the same air enters the turbine at 311 K and 150...
NGINEERI 13. A centrifugal compressor (not a piston type) compresses the air from the ambient condition at T, 300K and Pi 1 bar to P 10 bar following three different, standalone paths: isentropic,...
NGINEERI 13. A centrifugal compressor (not a piston type) compresses the air from the ambient condition at T, 300K and Pi 1 bar to P 10 bar following three different, standalone paths: isentropic, reversible isothermal, and an irreversible adiabatic process, respectively. (Note: These processes are not sequential processes; rather each of them is an independent, standalone p They all start at the same initial condition at state 1, but they end at different state 2.) The mass flow rate is...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and 300 K to an exit pressure of 900 kPa. Determine the compressor work per unit mass for (a) isentropic compression with k 1.4, (b) a compressor with 85% isentropic efficiency, (c) two-stage compression (100 kPa to 300 kPa, and 300 kPa to 900 kPa) with intercooling with an isentropic efficiency of 85% for both compressors. (50 points) 2.
Question 10 10 pts A gas turbine operates with a two stage air compressor incorporating intercooling,...
Question 10 10 pts A gas turbine operates with a two stage air compressor incorporating intercooling, the pressure ratio and the air inlet temperature of 20°C is the same for both stages. The overall compression ratio is 10:1. The isentropic efficiency of both stages is 89.0% For air take y=1.4 and Co=1.005 KJ/kg.k Determine the specific work required to drive both compressors, your answer should be in KJ/kg to 1 decimal place. DO NOT INCLUDE UNITS IN YOUR ANSWER 5...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and 300 K to an exit pressure of 900 kPa. if the volume flow rate = 1 m/sec Determine: the compressor power (kW) for isentropic compression with k = 1.4 Choose... the compressor power (kW) for polytropic compression with n = 1.3 Choose.. the compressor power (kW) for ideal two stage compression with intercooling with a polytropic exponent of 1.3 Choose... the compressor power (kW)...
Brayton cycle question Problem 5 A Brayton cycle operates with a two stage compressor with an...
Brayton cycle question
Problem 5 A Brayton cycle operates with a two stage compressor with an intercooler and a two stage turbine with a reheater at an overall pressure ra- tio of 16. The cycle breaths in air from the surroundings at 100kPa and 20°c. Enough heat is added in the combustor so that the maximum temperature of this cycle is 940K. The intercooler reduces the temperature of the working luid to the air inlet temperature, and the reheater raises...
Air is compressed steadily by a reversible compressor from 100 kPa and 300 K to 900...
Air is compressed steadily by a reversible compressor from 100
kPa and 300 K to 900 kPa by a 10-kW motor. Assume air is both ideal
and has constant specific heat capacity values determined at room
temperature from Table A-2 at room temperature (300 K).
a) Determine the mass flow rate through the compressor if the
process is isentropic. ( find and identify the work per unit
mass)
b) polytropic with n = 1.2
c) isothermal
d) ideal two-stage polytropic...
Given: Air at 20 C and 100 kPa enters the first stage, and it exits the third stage at 6400 kPa. An inter-cooler is used to cool the air between the stages back to 20°C. The compression work per unit mass of air is γ-1 where γ is the specific heat ratio, R is the gas constant, subscript "i" denotes the initial (atmospheric) conditions, and subscript "o" signifies the exiting conditions. Find: intermediate pressures so that the total work is...
Air enters a two-stage compressor at 300 K and 101 kPa. The pressure ratio of each compressor stage is 3, and there is intercooling between the stages, which reduces the temperature of the air back to 300 K. The efficiency of the compressors is 0.70; the ratio of specific heats for air, k, is 1.40; and the specific heat at constant pressure, p, is 1000 J/kg K. What would be the temperature of the air after the second compression if...
NGINEERI 13. A centrifugal compressor (not a piston type) compresses the air from the ambient condition at T, 300K and Pi 1 bar to P 10 bar following three different, standalone paths: isentropic, reversible isothermal, and an irreversible adiabatic process, respectively. (Note: These processes are not sequential processes; rather each of them is an independent, standalone p They all start at the same initial condition at state 1, but they end at different state 2.) The mass flow rate is...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and 300 K to an exit pressure of 900 kPa. Determine the compressor work per unit mass for (a) isentropic compression with k 1.4, (b) a compressor with 85% isentropic efficiency, (c) two-stage compression (100 kPa to 300 kPa, and 300 kPa to 900 kPa) with intercooling with an isentropic efficiency of 85% for both compressors. (50 points) 2.
Question 10 10 pts A gas turbine operates with a two stage air compressor incorporating intercooling, the pressure ratio and the air inlet temperature of 20°C is the same for both stages. The overall compression ratio is 10:1. The isentropic efficiency of both stages is 89.0% For air take y=1.4 and Co=1.005 KJ/kg.k Determine the specific work required to drive both compressors, your answer should be in KJ/kg to 1 decimal place. DO NOT INCLUDE UNITS IN YOUR ANSWER 5...
Air is compressed steadily by a reversible compressor from an inlet state of 100 kPa and 300 K to an exit pressure of 900 kPa. if the volume flow rate = 1 m/sec Determine: the compressor power (kW) for isentropic compression with k = 1.4 Choose... the compressor power (kW) for polytropic compression with n = 1.3 Choose.. the compressor power (kW) for ideal two stage compression with intercooling with a polytropic exponent of 1.3 Choose... the compressor power (kW)...
Brayton cycle question
Problem 5 A Brayton cycle operates with a two stage compressor with an intercooler and a two stage turbine with a reheater at an overall pressure ra- tio of 16. The cycle breaths in air from the surroundings at 100kPa and 20°c. Enough heat is added in the combustor so that the maximum temperature of this cycle is 940K. The intercooler reduces the temperature of the working luid to the air inlet temperature, and the reheater raises...
Air is compressed steadily by a reversible compressor from 100
kPa and 300 K to 900 kPa by a 10-kW motor. Assume air is both ideal
and has constant specific heat capacity values determined at room
temperature from Table A-2 at room temperature (300 K).
a) Determine the mass flow rate through the compressor if the
process is isentropic. ( find and identify the work per unit
mass)
b) polytropic with n = 1.2
c) isothermal
d) ideal two-stage polytropic...
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