EXAMPLE PROBLEMS FOR MIDTERM I.

Slides:



Advertisements
Similar presentations
Jet Engine Design Idealized air-standard Brayton cycle
Advertisements

Jet Engine Design diffuser compressor combustion chamber turbine nozzle P=constant q out q in T s 1-2 Isentropic compression in.
İsmail ALTIN, PhD Assistant Professor Karadeniz Technical University Faculty of Marine Sciences Department of Naval Architecture and Marine Engineering.
EGR 334 Thermodynamics Chapter 9: Sections 1-2
Internal Combustion Engines. Ideal Diesel Cycle Ideal Diesel Cycle.
EXERCISE 1 CHAPTER 12.
EXERCISE 1 CHAPTER 11.
Unit Four Quiz Solutions and Unit Five Goals
Specific Heat Thermodynamics Professor Lee Carkner Lecture 8.
Thermodynamics Professor Lee Carkner Lecture 18
For next time: Read: § 8-6 to 8-7 HW11 due Wednesday, November 12, 2003 Outline: Isentropic efficiency Air standard cycle Otto cycle Important points:
How much work is done when the ideal gas is expanded from V 1 to V 2 at constant pressure? A] 0 B] nRT 2 C] nRT 1 D] nR(T 2 -T 1 ) E] it depends on whether.
EGR 334 Thermodynamics Chapter 9: Sections 7-8
INTERNAL COMBUSTION ENGINES (reciprocating). Geometry.
Thermodynamic Cycles Air-standard analysis is a simplification of the real cycle that includes the following assumptions: 1) Working fluid consists of.
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
EGR 334 Thermodynamics Chapter 9: Sections 5-6
Thermodynamic Cycles for CI engines In early CI engines the fuel was injected when the piston reached TC and thus combustion lasted well into the expansion.
What happens when we change the quantity of gas
TUTORIAL 1.
Entropy of a Pure Substance Entropy is a thermodynamic property, the value of entropy depends on the state of the system. For example: given T & P, entropy,
Thermodynamic Cycles for CI engines
ME 200 L35 Ground Transportation (Air Standard Otto Cycle) 9.1 and 9.2 Material not picked up this week may be recycled! ME 200 L35 Ground Transportation.
TEKNIK PERMESINAN KAPAL II (Minggu – 3) LS 1329 ( 3 SKS) Jurusan Teknik Sistem Perkapalan ITS Surabaya.
INTERNAL COMBUSTION ENGINES LECTURER PROF.Dr. DEMIR BAYKA.
MT 313 IC ENGINES LECTURE NO: 04 (24 Feb, 2014) Khurram Yahoo Group Address: ICE14.
AR Thermodynamics I Fall 2004 Course # 59:009 Chapter 9, Section 2 Professor Ratner.
AREN 2110: WATER PROPERTIES
Example from Lecture 6 A stoichiometric mixture of air and gaseous methane at 54 o C and 2 bar is buried in a 0.1 m 3 rigid vessel. The temperature of.
Diesel Cycle and the Brayton Cycle Chapter 9b. Rudolph Diesel  German inventor who is famous for the development of the diesel engine  The diesel engine.
Internal combustion engines
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
APPLIED THERMODYNAMICS UNIT- 2 Gas power cycle 1 Department of Mechanical Engineering,A.I.E.T.,Mijar 3)Air Standard Diesel Cycle/ Constant Pressure cycle:
ENGR 2213 Thermodynamics F. C. Lai School of Aerospace and Mechanical Engineering University of Oklahoma.
CHAPTER 3 The First Law of Thermodynamics: Closed Systems.
Chapter 4 ENERGY ANALYSIS OF CLOSED SYSTEMS
What volume will 1 mole of a gas occupy at STP? STP = 273K, 1.013x10 5 Pa One mole of any ideal gas occupies a volume of 22.4L at STP.
THERMODYNAMIC ANALYSIS OF IC ENGINE Prepared by- Sudeesh kumar patel.
The Otto Cycle for a 4 stroke gasoline engine.
Gas Power Cycles.
Introduction to Food Engineering
CHAPTER 3 ENERGY ANALYSIS OF CLOSED SYSTEMS
A. Diesel cycle : The ideal cycle for CI engines
Unit 61: Engineering Thermodynamics
Chapter: 08 POWER CYCLES.
Power Plant Technology Combined Cycle and Renewable Energy Power Systems (Assignment 1) by Mohamad Firdaus Basrawi, Dr. (Eng) Mechanical Engineering Faculty.
SPECIFIC HEATS The specific heat is defined as the energy required to raise the temperature of a unit mass of a substance by one degree. In general, this.
ES 211:Thermodynamics Tutorial 10
CHAPTER 4: Energy Analysis of Closed Systems
Power Plant Technology Steam and Gas Cycle Power Plant (Assignment 2)
Air standard cycles vs actual performance. With a compression ratio of 7:1, the actual indicated thermal efficiency of an SI engine is of the order of.
Fuel-Air Modeling of IC Engine Cycles - 1
Chapter 5 The First Law of Thermodynamics for Opened Systems
SI Engine Cycle Actual Cycle Intake Stroke Compression Power Exhaust
Chapter 7 Entropy: A Measure of Disorder
Thermo-Economic Analysis of Otto Cycle
FIRST LAW ANALYSIS OF COMBUSTION SYSTEMS
Ideal Diesel and Dual Cycles for I.C. Engines
Analysis of Constant Pressure Steam Generation
Ideal Diesel and Dual Cycles for I.C. Engines
Energy Analysis of Closed Systems
Chapter 3 Properties of Engineering Working Fluid
20th Century Thermodynamic Modeling of Automotive Prime Mover Cycles
Example 3 (A poorly maintained system)
Ideal Otto Cycles for I.C. Engines
Thermodynamics Lecture Series
Thermodynamics Lecture Series
Thermodynamic Analysis of Internal Combustion Engines
Chapter 6 ENERGY ANALYSIS OF CLOSED SYSTEM
Presentation transcript:

EXAMPLE PROBLEMS FOR MIDTERM I

PROBLEM 1 For an air standard ideal Otto cycle the pressure and temperature at the beginning of compression are 90 kPa and 300 K respectively. The temperature at the end of heat input at constant volume is 2300 K. The compression ratio is 9.5. (R = 0.287 kJ/kg-K and Cp = 1.005 kJ/kg-K for the whole cycle) Calculate; The work done during compression. b) The work done during expansion c) The mean effective pressure

The logic of the solution will be from TOP to BOTTOM 1 2 3 4 P v GIVEN P1 = 90 kPa T1 = 300 K R = 0.287 kJ/kg-K Cp = 1.005 kJ/kg-K R = 9.5 T3 = 2300 K REQUIRED Wc = ? SOLUTION The logic of the solution will be from TOP to BOTTOM The solution will be from BOTTOM to TOP

k = 1.4 T2 = 738 K T4 = 935 K Cv = 0.718 kJ/kg-K v1 = 0.956667 m3/kg v2 = 0.1007 m3/kg vs = 0.8560 m3/kg Wcomp = -314 kJ/kg Wexp = 980 kJ/kg Wnet = 666 kJ/kg Pe = 778 kJ/kg

Problem 3 The temperature and pressure of the reactants at the beginning of compression in an otto cycle is 25 C and 90 kPa respectively. The temperature and pressure of the reactants at the end of compression is 320 C and 1500 kPa. The fuel used is gasoline (C7.76H13.1) and the excess air coefficient is 0.9. Find the heat lost per kg of reactants, during compression. The mean molar specific heat of the reactants during compression. b) The mean specific heat of the reactants per kg of mixture, during compression c) The change of the internal energy of the reactants during compression. d) The work done on the reactants during compression e) The heat lost by the reactants during compression.

1 2 3 4 P v

Air-standard dual cycle r = 15 Pmax = 10 Mpa Qv = 0,2 Qin Qp = 0,8 4 REQUIRED hth = ? GIVEN Air-standard dual cycle r = 15 Pmax = 10 Mpa Qv = 0,2 Qin Qp = 0,8 P1 = 0,1 MPa T1 = 320 K 44 1 2 3 4 5

SOLUTION v1 = 0,9184 m3/kg v2 = 0,061227 m3/kg T2 = 945 K P2 = 4431 kPa T3 = 1707 K Qv = 546 kJ/kg Qp = 2185 kJ/kg T4 = 3882 K v4 = 0,1114 m3/kg d = 8,24 T5 = 1670 K Qout = 1356 kJ/kg hth = 0,50