Show the complete solution An engine operates on an Otto cycle with a compression ratio of 8. At the beginning of theisentropic compression process, the volume, pressure and the temperature of the air are 0.01m³, 110 kPa, and 50°C, respectively. At the end of the combustion process, the temperature is900°C. Find (A) the temperature at the remaining two states of the Otto cycle, (B) the pressureof the gas at the end of the combustion process, (C) heat added per unit mass to the engine inthe combustion chamber, (D) heat removed per unit mass from the engine to the environment,(E) the compression work per unit mass added, (F) the expansion work per unit mass done, (G)MEP, and (H) thermal cycle efficiency. [ANSWERS: (A) 469.3°C, 237.5°C, (B) 2022 kPa,(C) 3.67 kJ/kg, (D) -1.60 kJ/kg, (E) -300.5 kJ/kg, (F) 474.8 kJ/kg, (G) 236.6 kPa, (H) 56.47%]

As per Expert Guidelines, we are supposed to answer only the first three sub-parts of the given…

Answered: An engine operates on an Otto cycle…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

i need the answer quickly
a petrol working on a constant volume cycle has a compression ratio of 9 to 1. if the pressure and temperature of the petrol-vapor mixture at the beginning of compression assuming it follows the law PV^1.4=C
3. In a cycle, a 4kg ideal gas (MW=3g/mol and k=2.3) confined in a controlled mass system went through three processes. The gas was started at 20kPa and 310K in the first process, and it was isometrically increased by 30kPa. The gas was subjected to 400K using a process defined by PV^3=C. It returns to its original state polytropically. Calculate the entropy change for each process.
1. In a constant temperature closed system process, 100 Btu of heat is transferred to the working fluid at 100 °F. What is the change of entropy of the working fluid?
Required information Problem 07.021 - DEPENDENT MULTI-PART PROBLEM - ASSIGN ALL PARTS NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. During the isothermal heat addition process of a Carnot cycle, 700 kJ of heat is added to the working fluid from a source at 400°C. Problem 07.021.c - Total entropy change for the process Determine the total entropy change for the process. The total entropy change for the process is KJ/K.
QIAt the commencement of the compression stroke, the cylinder of an oil engine is charged with air at 96.5kPa and 65°C. Compression takes place to 1/14th of the original volume according to the law PV.35 =C. Fuel the injected, the mass of the fuel injected being 1/40th of that of the air in the cylinder, and combustion takes place at constant pressure. Taking t5he calorific value of the oil as 44000OKJ/kg, determine a- the theoretical pressure and temperature after compression b- the theoretical temperature after combustion c- the fraction of the stroke at which combustion is theoretically complete, cp=1.003KJ/kg.K (3400kPa, 579°C, 1649°C, 0.0967)
Consider an air-standard Otto cycle. At the beginning of the compression process, the pressure and temperature are 100 kPa and 300 K. The displacement volume is 2 liters, compression ratio is 10 and the pressure at the end of the combustion is 4 times the pressure at the end of the compression.Use cold-air standard calculations and determine the pressure, temperature and volume at each state and fill in the below table:
4. Steam at a temperature of 210°C has a specific entropy of 7.1167 kJ/kg.K. Determine the pressure, internal energy, enthalpy and volume.
A four-cylinder, four-stroke, 1.6-L gasoline engine operates on the Otto cycle with a compression ratio of 11. The air is at 100 kPa and 37°C at the beginning of the compression process, and the maximum pressure in the cycle is 8 MPa. The compression and expansion processes may be modeled as polytropic with a polytropic constant of 1.3. Using constant specific heats at 850 K, determine the specific fuel consumption, in g/kWh, defined as the ratio of the mass of the fuel consumed to the net work produced. The air– fuel ratio, defined as the amount of air divided by the amount of fuel intake, is 16.
In an air-standard Brayton cycle the air enters the compressor at 0.1 MPa and 15°C. The pressure leaving the compressor is 1.0 MPa, and the maximum temperature in the cycle is 1100°C. Determine the pressure and temperature at each point in the cycle and the compressor work, turbine work, and cycle efficiency. For each of the control volumes analyzed, the model is ideal gas with constant specific heat, at 300 K, and each process is steady state with no kinetic or potential energy changes
One mole of an ideal monatomic gas, occupying 5 L at 3270 °C, is carried through a Carnot cycle. It is first expanded isothermally to a volume of 25 L and then adiabatically to a stage at which the temperature is 270 °C. It is then compressed isothermally to a certain volume and then finally back to the initial state. Calculate the quantities of AE, q and W in each step. Then calculate the efficiency.
One kilogram of a perfect gas (air) is used as a working substance in a Carnot power cycle. At thebeginning of isentropic compression, the temperature is 326 o K and the absolute pressure is 359 kPa. Theabsolute pressure at the end of the isentropic compression is 1,373 kPa. For this cycle, the isothermalexpansion ratio (v 3 /v 2 ) is 2.0. For the cycle, calculate the heat supplied, kJ/kg.A., heat rejected, and the network

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS