ME 475/675 Introduction to Combustion

Slides:



Advertisements
Similar presentations
ME 525: Combustion Lecture 3
Advertisements

Lecture 36 Combustion Reactions.
Course Outline Fundamentals and Combustion Systems Part I Chemical Equilibrium Chemical Kinetics Fuels Part II Flames Gas-Fired furnace combustion Premixed-charge.
AME 436 Energy and Propulsion Lecture 3 Chemical thermodynamics concluded: Equilibrium thermochemistry.
Combustion Calculations
Review of Chemical Thermodynamics Combustion MECH 6191 Department of Mechanical and Industrial Engineering Concordia University Lecture #1 Textbook: Introduction.
First Law of Thermodynamics
1st & 2nd Law Analysis for Combustion Process
ME 475/675 Introduction to Combustion Lecture 9. Announcements Midterm 1 September 29, 2014 (two weeks from today) HW 3 Ch 2 (57), Due now HW 4 Due Monday,
ME 475/675 Introduction to Combustion
Heat of Reaction 1st Law Analysis of Combustion Systems
1 MAE 5310: COMBUSTION FUNDAMENTALS Adiabatic Combustion Equilibrium Examples September 19, 2012 Mechanical and Aerospace Engineering Department Florida.
1 Equilibrium Composition of Flames 朱 信 Hsin Chu Professor Dept. of Environmental Engineering National Cheng Kung University.
Chapter 15 CHEMICAL REACTIONS
1 Chemical Equilibrium In general the combustion products consist of more than just CO 2, H 2 O, O 2, and N 2 For rich mixtures CO also exists in the products.
Chapter 16 Chemical and Phase Equilibrium Study Guide in PowerPoint to accompany Thermodynamics: An Engineering Approach, 5th edition by Yunus.
ME 475/675 Introduction to Combustion Lecture 8. Announcements.
Chemical Reaction Equilibria
Joshua Condon, Richard Graver, Joseph Saah, Shekhar Shah
Final Exam Review. Oxoacids Central element, surrounded by oxygens e.g. (not all listed) Recognizing Acids Hydrohalic Acids Group 7 ion with H+ HF, HCl,
ME 475/675 Introduction to Combustion Lecture 4. Announcements Extra Credit example due now HW 1 Due Friday Tutorials Wednesday 1 pm PE 113 Thursday 2.
ME 475/675 Introduction to Combustion
1 Adiabatic Flame Temperature Reaction Q W P 2 =P a T 2 =T a Consider the case where the cylinder is perfectly insulated so the process is adiabatic (
EGR 334 Thermodynamics Chapter 12: Sections 1-4
MAE 5310: COMBUSTION FUNDAMENTALS
Lecture #26 What’s on the Final?
WCB/McGraw-Hill © The McGraw-Hill Companies, Inc.,1998 Thermodynamics Çengel Boles Third Edition 14 CHAPTER Chemical Reactions.
Reacting Mixtures and Combustion
ENERGY CONVERSION ES 832a Eric Savory Lecture 7 – Energy of formation and application of the first law Department.
© 2014 Carl Lund, all rights reserved A First Course on Kinetics and Reaction Engineering Class 19.
INTERNAL COMBUSTION ENGINES LECTURER PROF.Dr. DEMIR BAYKA.
Gas Stoichiometry. Equal volumes of gases at the same temperature and pressure contain equal amounts of particles The coefficients in a balanced equation.
1 Fluid Models. 2 GasLiquid Fluids Computational Fluid Dynamics Airframe aerodynamics Propulsion systems Inlets / Nozzles Turbomachinery Combustion Ship.
ENERGY CONVERSION ES 832a Eric Savory Lecture 6 – Basics of combustion Department of Mechanical and Material Engineering.
ENERGY CONVERSION ES 832a Eric Savory Lecture 6 – Basics of combustion Department of Mechanical and Material Engineering.
(12) The expression of K in terms of fugacity coefficient is: The standard state for a gas is the ideal-gas state of the pure gas at the standard-state.
ENERGY CONVERSION ES 832a Eric Savory Lecture 7 – Energy of formation and application of the first law Department.
Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Review for Final Exam See also: Exam 1 prep Exam 2 prep Exam 3 prep.
1 MAE 5310: COMBUSTION FUNDAMENTALS Lecture 2: Thermochemistry Review August 25, 2011 Mechanical and Aerospace Engineering Department Florida Institute.
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.
Power Plant Engineering
Review -1 School of Aerospace Engineering Copyright © by Jerry M. Seitzman. All rights reserved. AE/ME 6766 Combustion AE/ME 6766 Combustion:
Chapter 13: Gases. Nature of gases Assumptions of Kinetic-Molecular theory are based on four factors: 1)Number of particles present 2)Temperature 3)Pressure.
When gases react, the coefficients in the balanced chemical equation represent both molar amounts and relative volumes. Section 3: Gas Stoichiometry K.
Do Now 1.What is reaction rate? 2.What does the term “equilibrium” signify? Can you describe physical changes in the chemistry lab where equilibrium is.
CHAPTER 15 CHEMICAL REACTIONS Lecture slides by Mehmet Kanoglu Copyright © The McGraw-Hill Education. Permission required for reproduction or display.
ME 475/675 Introduction to Combustion
ME 475/675 Introduction to Combustion
MAE 5310: COMBUSTION FUNDAMENTALS
ME 475/675 Introduction to Combustion
MAE 5310: COMBUSTION FUNDAMENTALS
INTRODUCTION Motivation
Problem 1 Diesel fuel (C12H26) at 25 ºC is burned in a steady flow combustion chamber with 20% excess air which also enters at 25 ºC. The products leave.
ME 475/675 Introduction to Combustion
ME 475/675 Introduction to Combustion
Gases React in Whole Number Ratios
ME 475/675 Introduction to Combustion
Engineering Thermodynamics
MAE 5310: COMBUSTION FUNDAMENTALS
Fluid Models.
Basic Chemistry Chapter 11 Gases Chapter 11 Lecture
Gestão de Sistemas Energéticos 2016/2017
Gas Stoichiometry.
Basic Chemistry Chapter 11 Gases Chapter 11 Lecture
WCB/McGraw-Hill © The McGraw-Hill Companies, Inc.,1998 Thermodynamics Çengel Boles Third Edition 15 CHAPTER Chemical and Phase Equilibrium.
Stoichiometry of Gases
Pure Substance and Two property Rule
COMBUSTION THERMODYNAMICS DEEPA M S & VARUNA TANDON
Presentation transcript:

ME 475/675 Introduction to Combustion Lecture 10 Next year give next lecture here and this lecturer next time. Ask students to attempt HW before coming to this lecture Examples using Computer Programs and Constant Specific Heats

Announcements FALL 2017 CAREER FAIR Midterm 1 HW 4 Thursday, September 28 Learn more about career services Midterm 1 October 2, 2017 HW 4 Due Friday (I’ll accept it Monday) Ch 2 (33, 47, 57, 50, 54, 63)

Problem 2.47 (homework) Calculate the equilibrium composition for the reaction 𝐻 2 + 1 2 𝑂 2 ↔ 𝐻 2 𝑂 when the ratio of the number of moles of elemental hydrogen to elemental oxygen is unity. The temperature is 2000 K, and the pressure is 1 atm. Extra: What will happen to the amount of 𝐻 2 if the pressure is decreased? At what pressure will 𝜒 𝐻 2 =0.01?

Problem 2.50 (homework) Reformulate problem 2.47 to include the species OH, O, and H. Identify the number of equations and the number of unknowns. They should of course be equal. (Write a system of equations that can be used to solve for the unknowns). Do not solve your system.

Problem 2.54 (Homework) Consider the combustion of decane (C10H22) with air at an equivalence ratio of 1.25, pressure of 1 atm, and temperature of 2200 K. Estimate the mixture composition assuming no dissociation except for the water-gas shift equilibrium. Compare with results of TPEQUIL. Hint: Hydrocarbon Combustion with Shift Reaction Equilibrium MathCAD Solution www.mhhe.com/turns3e

Problem 2.63 (Homework) A furnace uses preheated air to improve its fuel efficiency. Determine the adiabatic flame temperature when the furnace is operating at a mass air-fuel ratio of 16 for air preheated to 600 K. The fuel enters at 200 K. Assume the following simplified thermodynamic properties: Tref = 300 K, MWfuel = MWair = MWprod = 29 kg/kmol; cp,air = cp,prod = cp,fuel = 1200 J/kg-K; ℎ 𝑓,𝑎𝑖𝑟 𝑜 = ℎ 𝑓,𝑝𝑟𝑜𝑑 𝑜 =0; ℎ 𝑓,𝑓𝑢𝑒𝑙 𝑜 =4∗ 10 7 𝐽/𝑘𝑔

Problem 2.33 (Homework) Once more, repeat problem 2.30, but eliminate the unrealistic assumptions, i.e. allow for dissociation of the products and variable specific heats. Use HPFLAME (Appendix F), or other appropriate software. Compare and contrast the results of problems 2.30 to 2.33. Explain why they differ. 2.30 Determine the adiabatic flame temperature for constant- pressure combustion of a stoichiometric propane-air mixture assuming reactant at 298K, no dissociation of the products, and constant specific heats evaluated at 298K. www.mhhe.com/turns3e

Problem 2.35 (homework) Repeat problem 2.30, but for constant-volume combustion. Also, determine the final pressures. Add, compare results with UVFLAME

Computer Programs Provided by Book Publisher Described in Appendix F For “complex” reactions (11 product species) Fuel: CNHMOLNK Oxidizer: Air Download from web: www.mhhe.com/turns3e student edition Computer codes Access to TPEquil, HFFlame, UVFlame Extract All TPEQUIL (TP Equilibrium) Use to find Equilibrium composition and mixture properties Required input Fuel CNHMOLNK Temperature Pressure Equivalence ratio (with air) to determine initial number of moles of each atom

HPFLAME (HP Flame) Use to find Required Input Adiabatic flame temperature for constant pressure Required Input Fuel, equivalence ratio, enthalpy of reactants HR, pressure For constant pressure: HP = HR Find TAd In our examples we assume ideal combustion so we knew the product composition But this program calculates the more realistic equilibrium composition of the products from a (complex) equilibrium calculation (multiple equilibrium reactions) But this requires TProd = TAd, which we are trying to find! Requires program (not humans) to iterate