A) Calculate the net work output per kmol fuel. In your analysis, assume that the fuel is introduced as a gas at 298K.
Now consider an Ideal Diesel Cycle that has the same compression ratio and produces the same net work output as in Problem 1. If the cycle has a cut-off ratio of 2:
B) Calculate the required heat input per unit mass of air.
C) Find the temperature at each state of the cycle.
Homework Answers
Add Answer to:
A) Calculate the net work output per kmol fuel. In your analysis, assume that the fuel is introdu...
Problem 1 (65 pts): The cylinder of a Diesel engine is initially filled with air at 100 kPa and 2...
Problem 1 (65 pts): The cylinder of a Diesel engine is initially filled with air at 100 kPa and 298 K (piston is at BDC). The air is then compressed isentropically with a compression ratio of 20. Fuel, n-dodecane, is then introduced and combusted with the air, which produces work output (i.e. pushes the piston back to BDC). At the end of the power stroke, the temperature of the combustion products is 1020 K. The amount of heat lost to...
Step 3: Fuel Delivery at Max Power: At maximum output, calculate what the fuel-per-cycle quantity...
compression ratio is 8.8:1, not sure what the question is
asking
Step 3: Fuel Delivery at Max Power: At maximum output, calculate what the fuel-per-cycle quantity would be by using a 15:1 air-fuel ratio (Otto) or 22:1 (Diesel), based on the maximum mass contained in your combustion chamber. Note that the mass of air can be found using the ideal gas law and your initial conditions (ambient for an NA engine, for example). For force-fed
Step 3: Fuel Delivery at...
2. Analyze an Audi 3.0-liter TDI V6 Biturbo diesel engine using an air-standard Diesel cycle that...
2. Analyze an Audi 3.0-liter TDI V6 Biturbo diesel engine using an air-standard Diesel cycle that addresses the "real" effects of non-isentropic compression/expansion, air-fuel ratio, fuel heating value, incomplete combustion, exhaust residual, and heat loss. The engine is four-stroke, has six cylinders with a compression ratio of 16.0, and develops maximum power at 4250 rpm. Assume the following: the diesel fuel heating value is Quv 42,600 kJ/kg, the air-to-fuel ratio (AF) at maximum power is 25, and the combustion efficiency...
Define thermodynamic States 1-7 in terms of u,v,T,P,S State Piston position BDC TDC TDC Conditions Air...
Define thermodynamic States 1-7 in terms of u,v,T,P,S State Piston position BDC TDC TDC Conditions Air and fuel at a known pressure and temperature After isentropic compression from BDC to TDC After constant volume combustion at TDC. Assume the products are only CO2, H20, 02, and N2 After isentropic expansion from TDC to BDC. Assume the species are the same as state 3 4 BDC BDC TDC TDC For the engine given in the table below Number of cylinders Bore...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows:...
A Diesel engine is approximated by a pressure limited (dual)
cycle. The data is as follows:
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P1 = 100 kPa, T1 = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg/kgf 40% of the heat is added in the constant volume combustion part....
A compression ignition engine is being analyzed. The residual gas fraction is xr=0.02. The fuel-to-air equivalence ratio is...
A compression ignition engine is being analyzed. The residual gas fraction is xr=0.02. The fuel-to-air equivalence ratio is f=0.6. At the end of the compression stroke the temperature is T2=1300 K and specific volume is v2=0.19 m3/kg-air. The maximum cycle pressure is P3=4000 kPa. At the end of the power stroke the specific volume is 1.00 m3/kg-air. Calculate the temperature at the end of the combustion process, T3b, and calculate the work done [kJ/kg-air] during the power stroke.
The answer is: 26.3% and 56.48 hp. Problem 12: An actual four-stroke SI engine has a...
The answer is: 26.3% and 56.48 hp.
Problem 12: An actual four-stroke SI engine has a total cylinder volume of 0.0015 m3 and a compression ratio of 9:1. The engine runs at 3000 rpm. At the start of the compression stroke the air is at 303 K and a pressure of 100 kPa. The ratio of the actual thermal efficiency of the engine to the air-standard cycle efficiency is 45%. The air to fuel ratio is 13:1. The internal energy...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows:...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P1 = 100 kPa, T = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg/kgf 40% of the heat is added in the constant volume combustion part. k=1.3, CH = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure rise parameter...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows:...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P, = 100 kPa, T = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg./kgf 40% of the heat is added in the constant volume combustion part. k=1.3, Cv = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure rise parameter...
A four-stroke 2.0 Litre compression ignition engine operates on a Diesel cycle with a compression ratio...
A four-stroke 2.0 Litre compression ignition engine operates on a Diesel cycle with a compression ratio of 20 and a cut-off ratio of 1.8. Air is at 30°C and 100 kPa at the beginning of the compression process. It may be assumed that for the air, the specific heat, Cp and gas constant, R are 1.005 and 0.287 kJ/kg.K, respectively. Calculate: the temperature (K) of the air at the end of the following processes: (i) (a) compression (ii) combustion, (ii...
Problem 1 (65 pts): The cylinder of a Diesel engine is initially filled with air at 100 kPa and 298 K (piston is at BDC). The air is then compressed isentropically with a compression ratio of 20. Fuel, n-dodecane, is then introduced and combusted with the air, which produces work output (i.e. pushes the piston back to BDC). At the end of the power stroke, the temperature of the combustion products is 1020 K. The amount of heat lost to...
compression ratio is 8.8:1, not sure what the question is
asking
Step 3: Fuel Delivery at Max Power: At maximum output, calculate what the fuel-per-cycle quantity would be by using a 15:1 air-fuel ratio (Otto) or 22:1 (Diesel), based on the maximum mass contained in your combustion chamber. Note that the mass of air can be found using the ideal gas law and your initial conditions (ambient for an NA engine, for example). For force-fed
Step 3: Fuel Delivery at...
2. Analyze an Audi 3.0-liter TDI V6 Biturbo diesel engine using an air-standard Diesel cycle that addresses the "real" effects of non-isentropic compression/expansion, air-fuel ratio, fuel heating value, incomplete combustion, exhaust residual, and heat loss. The engine is four-stroke, has six cylinders with a compression ratio of 16.0, and develops maximum power at 4250 rpm. Assume the following: the diesel fuel heating value is Quv 42,600 kJ/kg, the air-to-fuel ratio (AF) at maximum power is 25, and the combustion efficiency...
Define thermodynamic States 1-7 in terms of u,v,T,P,S State Piston position BDC TDC TDC Conditions Air and fuel at a known pressure and temperature After isentropic compression from BDC to TDC After constant volume combustion at TDC. Assume the products are only CO2, H20, 02, and N2 After isentropic expansion from TDC to BDC. Assume the species are the same as state 3 4 BDC BDC TDC TDC For the engine given in the table below Number of cylinders Bore...
A Diesel engine is approximated by a pressure limited (dual)
cycle. The data is as follows:
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P1 = 100 kPa, T1 = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg/kgf 40% of the heat is added in the constant volume combustion part....
The answer is: 26.3% and 56.48 hp.
Problem 12: An actual four-stroke SI engine has a total cylinder volume of 0.0015 m3 and a compression ratio of 9:1. The engine runs at 3000 rpm. At the start of the compression stroke the air is at 303 K and a pressure of 100 kPa. The ratio of the actual thermal efficiency of the engine to the air-standard cycle efficiency is 45%. The air to fuel ratio is 13:1. The internal energy...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P1 = 100 kPa, T = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg/kgf 40% of the heat is added in the constant volume combustion part. k=1.3, CH = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure rise parameter...
A Diesel engine is approximated by a pressure limited (dual) cycle. The data is as follows: Inlet temperature and pressure: P, = 100 kPa, T = 298 K Compression ratio = 16:1 Heat added during combustion = 44000 kJ/kgfuel (please note that this value is per kg fuel) A/F = 23 kg./kgf 40% of the heat is added in the constant volume combustion part. k=1.3, Cv = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure rise parameter...
A four-stroke 2.0 Litre compression ignition engine operates on a Diesel cycle with a compression ratio of 20 and a cut-off ratio of 1.8. Air is at 30°C and 100 kPa at the beginning of the compression process. It may be assumed that for the air, the specific heat, Cp and gas constant, R are 1.005 and 0.287 kJ/kg.K, respectively. Calculate: the temperature (K) of the air at the end of the following processes: (i) (a) compression (ii) combustion, (ii...
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