9-2 An air-standard cycle is proposed which begins at an initial state of 47 C, 1.2...
A gasoline engine operates on the air standard Otto cycle. The air intake to the engine is at 300K and 95kPa (State 1). The air is compressed in the engine to an unknown pressure. Heat is then added during combustion at an amount of 1100 kJ/kg. At the end of the heat addition process, the temperature reaches 2200K. Compute the following: (a) the temperature at the end of the compression process, (b) the volumetric compression ratio of this engine, (c)...
A heat engine takes 0.262 mol of a diatomic deal gas around the cycle shown in the pV-diagram below. Process 1 → 2 is at constant volume, process 2-) 3 is adiabatic, and process 3-1 is at a constant pressure of P = 2.00 atm. The value of r for this gas is 1.4 2,7-600K T,-300 K T, 492 K 0 (a) Find the pressure and volume at points 1, 2, and 3. pressure (Pa) volume (m3) point 1 point...
Use engineering methodology and show units calculations.
An air standard Otto cycle at the initial condition of P,=1 bar, T,=290 °K, Vi= 400 cm?. The maximum temperature of the engine is 2200 °K and compression ratio is 8. The mass of air is assumed to be 4.8x104 kg. Assume isentropic process exits in both compression and expansion strokes. (a) Sketch the P-V and T-S diagram of the cycle (5%), (b) determine the total heat addition to the gas in kj...
15. An air-standard, ideal gas cycle with limited-pressure combustion is used to evaluate an ideal compression ignition engine. The compression ratio is 12. The maximum temperature in the cycle is 2040 °F. The minimum temperature and pressure in the cycle is 40 OF and 20 psia, respectively. The coefficient β=1.2 (β is the ratio of the volume after to the volume before the constant pressure heat input process). Calculate the heat added during combustion per lbm of air, and the...
An air standard Otto cycle at the initial condition of P,=1 bar, T,=290 °K, V = 400 cm². The maximum temperature of the engine is 2200°K and compression ratio is 8. The mass of air is assumed to be 4.8x104kg. Assume isentropic process exits in both compression and expansion strokes. (a) Sketch the P-V and T-S diagram of the cycle (5%), (b) determine the total heat addition to the gas in kj (20%). (c) Net cycle work output of the...
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An air-standard cycle with constant specific heats is executed in a closed system and is composed of the following four processes: 1-2 Isentropic compression from 100 kPa and 22°C to 600 kPa 2-3 v = constant heat addition to 1500 K 3-4 Isentropic expansion to 100 kPa 4-1 P= constant heat rejection to initial state Study the effect of varying the temperature after the constant-volume heat addition from 1500 K to 2500 K in steps of...
A system consisting of 1.0 kg of water and undergoes a thermodynamic power cycle composed of the following four processes: Process 1 – 2: Constant pressure heating at 1 MPa from saturated vapor Process 2 – 3: Constant volume cooling to pz = 500 kPa, Tz = 160°C Process 3 – 4: Isothermal compression with Q34 = -815.8 kJ Process 4-1: Constant volume heating (a) Sketch the cycle on T - v and p - v diagrams. (b) Is this...
At the beginning of the compression process of an air standard Otto cycle, p1 = 1 bar, T1 = 300 K. The maximum temperature in the cycle is 2250 K and the compression ratio is 9.8. The engine has 4 cylinders and an engine displacement of Vd = 2.7 L. Determine per cylinder: a) the volume at state 1. b) the air mass per cycle. c) the heat addition per cycle, in kJ. d) the heat rejection per cycle, in kJ. e) the net work...
B2. (15%) (Show all your calculation steps.) An air standard Otto cycle at the initial condition of P=1 bar, T.-290°K, Vi-400 cm. The maximum temperature of the engine is 2200 °K and compression ratio is 8. The mass of air is assumed to be 4.8x104kg. Assume isentropic process exits in both compression and expansion strokes. (a) Sketch the P-V and T-S diagram of the cycle (5%), (b) determine the total heat addition to the gas in kj (20%). (c) Net...
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...