3. for the diesel engine
gamma = 1.4
1-2 Adiabatic compression
2-3 Isobaric Expansion
3-4 Adiabatic Expansion
4-1 Isochoric Cooling
a. V1 = V
P1 = P
then for adiabatic compression
P1V1^1.4 = P2V2^1.4
P1/P2 = (V2/V1)^1.4 = (1/18)^1.4 = 0.017483102
also
P1V1 = nRT1
P2V2 = nRT2
T1/T2 = (P1/P2)(V1/V2) = 0.314695837
b. n = 0.1 mol
P1 = 1.01*10^5 Pa
T1 = 300 K
P1V1 = nRT1
V1 = 0.002468316 m^3
hence
V2 = V1/18 = 1.371287*10^-4 m^3
c. V3 = 3V2 = 4.1138*10^-4 m^3
for isobaaric expansion
heat supplied = Q = nCp(T3 - T2)
P3V3 = nRT3
P2V2 = nRT2
Q = nCp(V3 - V2)P2/nR
Cp - Cv = R
Cp/Cv = gamma
Cp - Cp/gamma = Cp(gamma - 1)/gamma = R
Cp = gamma*R/(gamma - 1)
Q = 1.4(2*1.371287*10^-4)*1.01*10^5/0.4*0.017483102
Q = 5545.3540738 J
Rebelmatk Cycle bewo Veas 3) The Diesel... .I mean, Rebelmatic engine is used in vehicles across...
An idealized diesel engine operates in a cycle known as the air-standard diesel cycle shown in the figure below. Fuel is sprayed into the cylinder at the point of maximum compression, B. Combustion occurs during the expansion B-C, which is modeled as an isobaric process. Show that the efficiency of an engine operating in this idealized diesel cycle is given by the following expression. (Submit a file with a maximum size of 1 MB.) 1/10-TA VTC e-1- Adiabatic processes V...
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 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...
Need help with this thermodynamics problem . You have an engine modeled after the Diesel cycle with a compression ratio of 12. The intake conditions of the air are 300 K, 400 cm, and 100 kPa. After compression, liquid n-Octane is injected and heating occurs at constant pressure. Choose a reasonable maximum temperature and analyze the cycle to find the net work (kl) done. You may do this in EES or use the perfect gas method. Note that this will...
QUESTION 2(25%) 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/kg 40% of the heat is added in the constant volume combustion part. k = 1.3, C, = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure...
QUESTION 2(25%) 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/kg 40% of the heat is added in the constant volume combustion part. k = 1.3, C, = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure...
QUESTION 2(25%) 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/kg 40% of the heat is added in the constant volume combustion part. k = 1.3, C, = 0.81 kJ/kg.K, isentropic expansion and compression Find the values of pressure...
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...
Consider the expansion stroke only of a typical air-standard Diesel cycle engine which has a compression ratio of 20 and a cutoff ratio of 2. At the beginning of the process (fuel injection) the air temperature is 627°C, and the air expands at a constant pressure of 6.2 MPa until cutoff (volume ratio 2:1). Subsequently the air expands adiabatically until it reaches the maximum volume. Using ideal gas properties of air at 1000K, determine the: (a) temperatures reached at the...
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...