Fundamentals of Combustion _NPTEL
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NPTEL Online - IIT Kanpur
Course Name Fundamental of Combustion Department
Aerospace Engineering, IIT Kanpur
Instructor
Dr. D.P. Mishra
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Question can never be silly, It can be like a beautiful lily, In the garden of knowledge, This is still a truth, age after age. - Dr. D.P. Mishra
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Module 1: Introduction to Combustion Lecture 1: Introduction The Lecture Contains: Introduction to Combustion What is Combustion? Combustion Triangle Applications of Combustion Contd..
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Module 1: Introduction to Combustion Lecture 1: Introduction
Introduction to Combustion Introduction
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Module 1: Introduction to Combustion Lecture 1: Introduction Combustion Triangle Essential conditions for combustion to occur 1. 2. 3. 4. 5.
Presence of fuel . Presence of oxidizer (Not essentially oxygen). They must be in right proportions. The proportion will be dictated by flammability limit. Ignition energy.
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Module 1: Introduction to Combustion Lecture 1: Introduction Applications of Combustion Power Plants Chemical Industries Domestic Burner Automobiles
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Module 1: Introduction to Combustion Lecture 1: Introduction Contd..
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? The Lecture Contains: What is Fuel and Oxidizer? Types of Fuels and Oxidizers Contd.. Characterization of a Gaseous Fuel Junker's Calorimeter Liquid Fuels and Oxidizers Refinery End-Products of Typical Crude Oil
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? What is Fuel and Oxidizer?
Electronegativity The ability of an element to accept or donate electrons. Amount of pull that one atom exerts on the electron that it is sharing with other atom. The term electronegativity was coined by Linus Pauling, a Noble Laureate. Electronegativity
Element
Electronegativity
Element
Electronegativity
F
4
Br
2.8
B
2.0
O
3.5
C,S,I
2.5
Be,Al
1.5
N,Cl
3.0
H,P
2.1
Mg
1.2
Element
Fluorine is having Highest Electronegativity (Most powerful oxidizer). Oxygen has second highest electronegativity. Carbon, Hydrogen, Aluminum and Magnesium have Low Electronegativity (Fuels).
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? Types of Fuels and Oxidizers
Gaseous Fuel and Oxidizer
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? Contd.. Types of Gaseous Fuel and Oxidizer Sl. No.
Fuel
Oxidizer
Application
1
LPG
Air/O2
Domestic Burner, Furnace
2
Natural Gas (NG)
Air/O2
IC Engines, Furnaces
3
Producer Gas
Air/O2
EC/IC Engines
4
CH4 , C 3 H 8 , H 2
Air/O2
EC/IC Engines
5
Biogas
Air/O2
EC/IC Engines, Burners
6
Acetylene
Air/O 2
Gas welding, Gas cutting * EC=External Combustion IC =Internal Combustion
Composition of Some Gaseous Fuels Fuel
CO2
O2
N2
CO
H2
CH4
C 2 H6
C 3 H8
LPG
-
-
-
-
-
-
-
70
30
Natural Gas
-
-
5
-
-
90
5
-
-
Producer Gas
8
0.1
50
23.2
17.7
1
-
-
-
Propane
-
-
-
-
-
-
2.2
97.3
0.5
Biogas
33
-
1
-
1
65
-
-
-
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C 4 H10
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? Characterization of a Gaseous Fuel Heating Value: Amount of heat released per unit volume when it undergoes oxidation at normal pressure and temperature (0.1 MPa and 298 K). Lower heating value (LHV) – amount of heat released by burning 1 kg of fuel assuming the latent heat of vaporization in the reaction products is not recovered.
Higher heating value (HHV) – heating value of the fuel when water is condensed. is the Latent heat of vaporization of water at 298.15 K
Junker's Calorimeter
(Figure 2.1)
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? Determines the heating value of the gaseous fuel. Fuel and air are burnt in a burner. Cooling water in the water jacket-absorbs the heat released during combustion. Heating value- calculated from the water flow rate and rise in temperature.
Liquid Fuels and Oxidizers Liquid fuel is one of the major energy sources in the transport sector. Crude oil is formed from organic sources, animals, vegetables – which are entrapped in rocks under high pressure and temperature for million years.
Fuel
Oxidizer
Application
1
Gasoline
Air
S.I. Engine, Aircraft Piston Engine
2
HSD
Air
C.I. Engine
3
Furnace Oil
Air
Furnaces
4
Kerosene
Air
Aircraft, Gas Turbine, Engines Ramjet, Domestic Burner
5
Alcohols
Air
I.C. Engine
6
Hydrazine, UDMH, MMH, Liquid Hydrogen, Triethyl Amine
7
Hydrogen, Kerocene
Liquid O 2 , RFNA (Red Fuming Nitric Acid) N2 O 4
Liquid propellant rocket Engines
Air
Ramjet/Scramjet
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Module 1: Introduction to Combustion Lecture 2: What is Fuel and Oxidizer? Refinery End-Products of Typical Crude Oil Crude oil undergoes several process in the refinery. Generally separation of petroleum constituents occur in the distillation column. Constituents of typical crude oil is shown below.
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Module 1: Introduction to Combustion Lecture 3: Fuels The Lecture Contains: Bomb Calorimeter Properties of Liquid Fuels Properties of Common Liquid Fuels Solid Fuels and Oxidizers Contd..
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Module 1: Introduction to Combustion Lecture 3: Fuels Bomb Calorimeter Used to determine the calorific value of the liquid fuel. Liquid is burnt in the bomb in the presence of oxygen at about 2.5 MPa . The change in temperature in the water bath provides the calorific value of the fuel.
(Figure 3.2)
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Module 1: Introduction to Combustion Lecture 3: Fuels Properties of Liquid Fuels Specific Gravity
: Ratio of mass density of fuel to mass density of water at the same temperature
Reference temperature for fuel and water: 288.8 K American Petroleum Institute (API) Scale:
Relation between APISG and HHV: For Gasoline
:
For Kerosene
:
Auto Ignition : The lowest temperature required to make the combustion self sustained without Temperature any external aid
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Module 1: Introduction to Combustion Lecture 3: Fuels Properties of Liquid Fuels Flash : Minimum temperature at which liquid fuel will produce sufficient vapors to form a Point flammable mixture with air. Indicates maximum temperature at which liquid fuel can be stored without any fire hazard. Fire : Minimum temperature at which liquid fuel produces sufficient vapors to form a flammable Point mixture with air that continuously supports combustion establishing flame instead of just flashing. Smoke : Measure of the tendency of a liquid fuel to produce soot. Point
Properties of Common Liquid Fuels Automotive Gasoline
Diesel Fuel
0.72 - 0.78
0.85
0.796
0.8 X 10 -6
2.5 X 10 -6
0.75 X 10 -6
303 - 576
483 - 508
338
423-473
442
Flash point (K)
230
325
284
311
325
Auto ignition temperature (K)
643
527
737
483
--
Stoichiometric air/fuel by weight
14.7
14.7
6.45
15
15.1
Heat of Vaporization (kJ/kg)
380
375
1185
298.5
--
Lower heating value (MJ/kg)
43.5
45
20.1
45.2
43.3
Fuel Type Specific gravity Kinematics viscosity @ 293 K (m 2 /s) Boiling point range (K) @ STP
Methanol Kerosene 0.82 3.626 X 10 -6
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ATF (JP8) 0.71 --
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Module 1: Introduction to Combustion Lecture 3: Fuels Solid Fuels and Oxidizers Solid Fuels:
(Figure 3.2) Constituents of Solid Fuel:
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Module 1: Introduction to Combustion Lecture 3: Fuels Contd.. Types of Solid Fuels and Oxidizers: S. No.
Fuel
Oxidizer
Applications
1
Biomass (Wood, Saw Dust, Rice Husk, Rice Straw, Wheat Straw, etc)
Air/O2
Domestic Burner, Engine With Producer Gas
2
Coal, Coke, Charcoal
do
do
3
Special Fuels Nitrocellulose (NC), HTPB, CTPB
Nitroglycerine, Ammonium Perchlorate , Ammonium Nitrate, Nitrogen Tetraoxide
Solid Propellant Rocket, Hybrid Rocket
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Module 1: Introduction to Combustion Lecture 4: Characterization of Solid Fuels The Lecture Contains: Oxygen, Water and Ash Content of Certain Solid Fuels Characterization of Solid Fuels Various Combustion Modes
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Module 1: Introduction to Combustion Lecture 4: Characterization of Solid Fuels Oxygen, Water and Ash Content of Certain Solid Fuels Moisture in Solid Fuel: 1. Free 2. Bound water Fuel moisture content will affect rate of combustion and overall efficiency. Ash: The inorganic materials, which remain as residue even after complete combustion. Ash content affects the performance of the combustion system. Ash content causes fouling of the boilers. Fuel
Oxygen (Dry, Ash-free) Moisture (Ash-free)
Ash (Dry)
Wood
40-45%
15-70%
0.1-1.0%
Peat
30-35%
70-90%
0.1-20%
Lignite coal
20-25%
20-30%
>5%
Bituminous coal
3-5%
10-5%
>5%
Anthracite coal
1-2%
2-4%
>5%
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Module 1: Introduction to Combustion Lecture 4: Characterization of Solid Fuels Characterization of Solid Fuels: Proximate Analysis: Used to determine the moisture content, volatile matter, fixed carbon and ash content in the solid fuel. To determine water content, few grams of fuel is heated around 378 K till it attains constant weight. Volatile matter is determined by heating the sample at 1173 K. Ultimate Analysis: Used to determine the major elemental composition of the solid fuel. Nitrogen content is determined by chemical method. Sulphur content is evaluated by burning the fuel to convert it into SO4 followed by precipitation method. Calorific value can be determined by bomb calorimeter.
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Module 1: Introduction to Combustion Lecture 4: Characterization of Solid Fuels Various Combustion Modes
Premixed Flame
: Fuel and oxidizer are mixed before actual combustion. Examples: Bunsen burner, LPG Stove
Diffusion Flame
: Fuel and oxidizer are mixed in the region where chemical reaction takes place.
Laminar and Turbulent : Based on the flow characteristics; Turbulent flow occurs in practical Flames combustion devices.
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion The Lecture Contains:
Scope of Combustion Image Sources
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion Scope of Combustion Industrial Process Thermal energy for process chemical plants, sugar industries, food processing industries are obtained through combustion. Iron, steel and other metals are produced from raw materials through combustion. Heat treatment and annealing of metals. Rotary kilns are used to produce Portlant cement.
Sugar Industry
Food Processing
Process Chemical Plant
Steel Plant (Figure 5.1)
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion Transportation Surface transport vehicles are operated by reciprocating IC Engines Gas turbine combustors are used widely in air and marine transportation sectors.
(Figure 5.2)
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion
Power Generation Most of the thermal power plants are operated by burning coal. Recently gas turbine power plants are coming up.
Fluidized Bed Power Plant
Coal Power Plant
Biomass Based Power Plant
Gas Turbine Power Plant (Figure 5.3)
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion Waste Disposal Combustion finds application in disposing waste materials. Incinerators are used to dispose domestic and industrial wastes. In modern hospitals, incinerators are used to dispose hospital wastes safely.
(Figure 5.4)
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion Fire Sometimes fire causes damage to life and property. Forest Fire: Damages natural resources and lives. Structural Fire: Damages property and human lives. Effective fire breakers should be designed and implemented to avoid fire hazard. By using proper construction materials, Fire hazard can be minimized. Marine life is very much affected by oil spill fire.
(Figure 5.5)
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Module 1: Introduction to Combustion Lecture 5: Scope of Combustion Environmental pollution Combustion of any fuel produces certain amount of emissions such as smoke, ash, soot, and other harmful gases. Major pollution generated in combustion system are CO, CO 2 , NO, NO 2 , SO2 , ash, etc. These are due to incomplete combustion and can be minimized by increasing the residence time of fuel-oxidizer mixture in the combustor. Sources
Particulates
Carbon Monoxide
Unburnt Hydrocarbon
Nitrogen Sulfur oxides dioxides
Transportation
7
79
60
15
6
Stationary Combustion Systems/Electricity
8
speed of sound at isochoric condition detonation attains infinite velocity Region III: In this region Hence
Therfore
in this region is imaginary and physically impossible
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weak
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Module 5: Premixed Flame Lecture 22: Introduction Laminar Premixed Flame
(Figure 22.6) (Figure 22.7) First laboratory premixed Glame burner : Invented by Robert Bunsen in 1855
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Module 5: Premixed Flame Lecture 22: Introduction
Luminous Zone
Flame radiation: 3300 to 4400 A°
(Figure 22.8)
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame
The Lecture Contains: Structure of 1D Premixed Flame Laminar Flame Theory Flame Thickness Burning Velocity Measurement Methods
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Structure of 1D Premixed Flame
Preheat zone: Negligibly small heat release Certain chemical reactions take place in this zone Reaction zone: most of the chemical energy is released in the form of heat Decomposition of fuel takes place, leading to intermediate radical formation Reaction zone is very thin as compared to the preheat zone. Temperature gradient and concentration gradient are high .
(Figure 23.1)
Recombination zone: CO 2 and H 2 O are formed; No heat release in this zone
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Laminar Flame Theory Assumptions: 1D, steady, inviscid flow. Flame is quite thin. Ignition temperature is very close to flame temperature. No heat loss including radiation; Adiabatic flame. Pressure difference across the flame is negligibly small. Binary diffusion, Fourier and Fick's law are valid. Unity Lewis number. Constant transport properties
(1)
Mass conservation: Species conservation:
Energy equation:
Fuel:
(2)
Oxidizer:
(3)
Product:
(4)
(5) Global reaction mechanism:
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(6)
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Laminar Flame Theory (Contd.) Heat release due to chemical reaction: (7) Now energy equation becomes
In the reaction zone, (8)
Boundary conditions (For preheat zone) (10) (11) Recasted energy preheat zone,
equation
for
Rewriting, E.g. (11). (9)
(12)
Heat transfer due to conduction is balanced by convective heat transfer.
(13)
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Laminar Flame Theory (Contd.) Combining equations (10) and (13), (14)
(15) Mean fuel burning rate can also be expressed as,
Also, (16)
(19) Expression becomes,
Combining equations (15) and (16),
for
burning
(17) Mean fuel burning rate per unit volume, (18)
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velocity
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Flame Thickness
Ignition temperature can be approximated as
The temperature gradient at the flame surface is
Flame thickness: (Figure 23.2) Where,
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Module 5: Premixed Flame Lecture 23: Structure of 1D Premixed Flame Burning Velocity Measurement Methods
(Figure 23.3) Flame front visualization Luminous photography Shadowgraph photography Schlieren Photography
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Module 5: Premixed Flame Lecture 24: Tube Method
The Lecture Contains: Tube Method Combustion Bomb Method Soap Bubble Method Stationary Flame Method (Bunsen Burner) Flat Flame Burner Effect of Equivalence Ratio on S L
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Module 5: Premixed Flame Lecture 24: Tube Method Tube Method
(Figure 24.1) Procedure:
Combustible mixture is filled in the tube On ignition at one end, the flame propagates through the tube
Features:
Inner dia of tube should be greater than the quenching diameter The flame is planar in the beginning and curved towards downstream, due to buoyancy Natural convection distorts the planar flame front due to difference in densities Friction at the tube wall is also a reason for parabolic shape of the flame
The burning velocity is given by
: Flame front velocity : Unburnt gas velocity
: Cross-sectional area of tube
: Flame surface area
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Module 5: Premixed Flame Lecture 24: Tube Method Combustion Bomb Method
(Figure 24.2)
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Module 5: Premixed Flame Lecture 24: Tube Method Soap Bubble Method
(Figure 24.3)
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Module 5: Premixed Flame Lecture 24: Tube Method Stationary Flame Method (Bunsen Burner)
(Figure 24.4)
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Module 5: Premixed Flame Lecture 24: Tube Method Flat Flame Burner
(Figure 24.5)
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Module 5: Premixed Flame Lecture 24: Tube Method Effect of Equivalence Ratio on S L
(Figure 24.6)
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L
The Lecture Contains: Effect of Oxygen Concentration on S L Effect of Initial Pressure and Temperature on S L Effect of Inert Additives Flame Extinction Flame Quenching Simplified Analysis for Quenching Diameter
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Effect of Oxygen Concentration on S L
(Figure 25.1)
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Effect of Initial Pressure and Temperature on S L
This relation is supported by experimental data n: Overall order of global chemical reaction for HC flames with for HC flames with for HC flames with
Pressure index, For
,
m
is
negative,
indicating burning velocity with decreasing pressure
increases
For
,
m
(Figure 25.2)
is
constant, indicating burning velocity is constant
For
,
m
is positive,
indicating burning velocity decreases with decrease in initial pressure
(Figure 25.3)
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Effect of Inert Additives
(Figure 25.4)
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Flame Extinction
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Flame Quenching Fuel
Oxidizer
SL (cm/s)
dq (mm)
CH4
Air
40
2.5
CH4
O2
C3 H8
Air
C3 H8
O2
C2 H2
Air
C2 H2
O2
0.2
CO
Air
2.8
H2
Air
H2
O2
0.3 45
2.0 0.25
140
210
0.8
0.5 0.2
Quenching diameter for various stoichiometric fuel-oxidizer ratio.
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Module 5: Premixed Flame Lecture 25: Effect of Oxygen Concentration on S L Simplified Analysis for Quenching Diameter
Rate of heat generated per unit volume
Heat generated in flame volume
Heat loss rate due to wall conduction
(Figure 25.5) Assuming linear temperature distribution in flame,
Quenching diameter
After simplification,
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Module 5: Premixed Flame Lecture 26: Flammability Limits
The Lecture Contains: Flammability Limits Effect of Pressure on Limit Mixture Ignition Flame Stabilization Flame Stabilization by Burner Rim Turbulent Premixed Flame
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Module 5: Premixed Flame Lecture 26: Flammability Limits Flammability Limits
Instrument to determine flammability limit
Vertical glass tube of 1.2 m length and 50 mm ID
(Figure 26.1)
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Module 5: Premixed Flame Lecture 26: Flammability Limits Effect of Pressure on Limit Mixture
(Figure 26.2)
Fuel
Oxidizer
Stoichiometry (% Fuel)
LFL (%)
UFL (%)
Methane
Air
9.5
5
15
Ethane
Air
5.6
2.8
12.4
Propane
Air
5.6
2.1
9.1
CO
Air
29.5
12
74.2
Hydrogen
Air
29.2
4
74.2
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Module 5: Premixed Flame Lecture 26: Flammability Limits Ignition
Energy generated in flame = Ensible enthalpy Mass
Substituting quenching diameter
Substituting flame thickness
Dependence on pressure
(Figure 26.3)
Fuel-Air
MIE (mJ)
Methane-air
0.47
Ethane-air
0.4
Butane-air
0.34
Acetylene-air
0.03
CO-air
0.05
Hydrogen-air
0.02
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Module 5: Premixed Flame Lecture 26: Flammability Limits Flame Stabilization Local gas flow velocity = Local burning velocity
(Figure 26.4)
(Figure 26.5)
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Module 5: Premixed Flame Lecture 26: Flammability Limits Flame Stabilization by Burner Rim
(Figure 26.6) Stability of flame front near the rim of Bunsen burner
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Module 5: Premixed Flame Lecture 26: Flammability Limits Turbulent Premixed Flame
(Figure 26.7)
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Module 5: Premixed Flame Lecture 27: Flame Stabilization
The Lecture Contains: Turbulent Flame Regimes The Borghi Diagram Turbulent Burning Velocity Wrinkled Laminar Flame Distributed Reaction Flamelet in Eddies
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Module 5: Premixed Flame Lecture 27: Flame Stabilization Turbulent Flame Regimes Turbulent Flame Regimes
Reynolds number for turbulent flame:
Chemical reaction time:
Chemical reaction time:
Damkohler number
If Da >> 1, fast chemistry regime If Da
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