Friday 18 September 2009

CONCEPTS OF THERMODYNAMICS AND ITS LAWS

When I joined IEC College of Engg & Technology in 1999, for the first time I heard of Richard Feynman & his style of writings. His three volume Lectures on Physics changed me permanently. The language was lucid and he told about the facts of Physics just like a thriller novel. I became a diehard fan of Physics and Feynman.
These piece of article on thermodynamic concept is an earnest try to tell about energy mechanics as a story.


"Dedicated to the teaching methodology of Richard Feynman"

. . . . . . . . . . . .©sarpyl

CONCEPTUAL IDEAS :

                                  If we want to analyze movement of energy over space, then we must define the space that would be used for the observation, we would call it as a SYSTEM, separated from the adjoining space that is known as "Surroundings", by a boundary that may be real or may be virtual depending upon the nature of the observation. The boundary is called as SYSTEM BOUNDARY.

                                  So we get a space of certain volume where ENERGY TRANSFER (movement of energy) is going on, what may or may not be real, and distinct, it may be virtual (in case of flow system ), again if real boundary exists, then it may be fixed (rigid boundary like constant volume system) or may be flexible (like cylinder-piston assembly). For a certain experiment the system and surroundings together is called UNIVERSE.

                                  The interface between the system & surroundings is called as "SYSTEM BOUNDARIES", which may be real & distinct in some cases where as some of them are virtual, but it may be real, solid and distinct.


ENERGY:

                                  Although we can't exactly define what is Energy, yet we can say how does Energy behave, even we can measure the change in energy of the system, we may say that Energy always posses the capability to do certain amount of work depending upon the form of Energy. We can also describe the different forms of Energy those can exist like potential energy, kinetic energy, chemical energy, binding energy, nuclear energy etc.

                                  Depending upon the capacity to do work, energy can be classified into different forms. If the energy is highly ordered then it is HIGH GRADE ENERGY, like Kinetic Energy, where as when Energy exists in a chaotic form we call it LOW GRADE ENERGY. Heat energy of a body arises due to random motions of the individual molecules. Hence we can say that HEAT ENERGY is related with the chaosness of the molecules, therefore, it is the most low grade energy.


HEAT TRANSFER :

                                  Through the boundary, a system and its surroundings can exchange energy between them, if allowed by the boundary properties. There are three modes of energy interaction a system and surroundings. If the boundaries are permeable to allow heat flow across it, then the energy transfer mode is called HEAT TRANSFER.

                                  When a system absorbs heat energy from the surroundings due to the temperature difference between system and surroundings the transfer of energy is named as HEAT TRANSFER.


WORK TRANSFER :

                                  When a system has a flexible or movable boundary then energy can be transfer by virtue of workdone. If there exists a pressure gradient between a system and its surroundings then work exchange takes place between the system and the surroundings as the flexible boundary moves to destroy the pressure gradient that exists between the system and the surroundings. So we would say the Energy Transfer due to pressure gradient is named as WORK TRANSFER.


MASS TRANSFER :

                                  For flow process in a open system, mass transfer takes place between system & surroundings which is the third type of Energy Transfer and named as Mass Transfer. Any open system has two passages for fluid flow. Through one passage, the mass of the working substance enters into the system and aptly named as INLET, while the second passage is used by the working fluid to flow out of the system and it is named as OUTLET. So, in open system mass flow occurs across the system and this phenomenon of mass inflow and outflow from the system is named as MASS TRANSFER between a system and it's boundaries.


CONCEPTS OF MASS :

                                  What is mass? Or we can say what is it to be a substance? Here, again we face the fundamental difficulty to define Mass accurately, although we know how it does behave, we can measure its value even, but it is really not clear what is mass made of. When Einstein equates mass in terms of energy, it defines mass as a form of energy but they are bound within the mass which again consists of elementary but composite particles named electron, proton & neutron. Proton, neutrons are made of QUARKS, which are the most fundamental particles of nature. Although Quarks are already well researched, and we know the most possible reason of the “confinement” phenomenon, still there exists a large number of physical phenomenon which can be explained using the “standard model of particle physics”.


PROPERTIES OF A SYSTEM :

                                  A system is characterized by the values of its properties. So the most logical question that would arise here would be about properties of a system. So what is a property of a system? It has been seen that every object that exists in this Universe possesses some physical & chemical characteristics, like size, shape, mass, energy, chemical composition, colors etc. Among these various characteristics, those are related with energy directly or indirectly are called as "thermodynamic functions". There are mainly two types of thermodynamic functions, which can be better described in mathematical terms as they are physical quantity and hence are measurable. Here we shall take a little hiatus (break) to know some facts about physical quantity.


                                   Physical characteristics are of two types. Any physical characteristics can be represented by the mathematical quantity and it is thus represented by mathematical functions. There may be two types of mathematical functions. When expressed in differential form, some of the functions become Exact differential and some of them produces In-exact differential form. The exact differential functions are called as thermodynamic properties. They are also known as “Point Functions”. Where as the in-exact differentials are called “Path Functions”


EQUILIBRIUM CONDITIONS :

                                   Every thermodynamic function are directly or indirectly measurable and when there is no energy transfer between the system and surroundings, then the value of the functions assume a certain value by which we can specify the state or condition of a thermodynamic system. So, the values are only measurable when they are not changing over a period of time. What does it implicate that the values of the thermodynamic functions are not continuously changing. When the values are not changing it indicates a stability of the state of the system over a certain periods of time. This stability of a system implies an Equilibrium condition. Each and every equilibrium states are distinct and they are specified by the distinct value of the properties of the system at that equilibrium conditions.


CONCEPTS OF A THERMODYNAMIC PLANE :

                                  A thermodynamics system is a bi-variate function. It means that to specify a thermodynamic system we need to specify the values of any two properties. One can also describe a thermodynamic system has two degrees of freedom. So, mathematically, we can say that any thermodynamic system at a certain equilibrium condition can be represented as a point on a two dimensional plane. The plane thus formed plotting thermodynamic properties along X and Y axes of a Cartesian Coordinate system is known as thermodynamic plane.

                                 A point on this plane represents a system at a thermodynamic equilibrium condition, which can be defined as a state which is time invariant when it is isolated from the surroundings. So, at equilibrium condition the values of different thermodynamic properties remain constant over a considerable amount of time.


EXTERNAL DISTURBANCES AND CHANGE OF STATE OF A SYSTEM:

                                 We have already know that when the values of different thermodynamic properties become stable we get an equilibrium state where no values of the properties can be changed without application of any external influences. But, what happens, when an external agency tries to change the values of the properties of the system. Here, what does it mean by "external influences"? What does it mean in real life? We know from our daily life experiences that any kind of external influences can be at last reduced to any kind of force only and the use of external influences always lead to an exchange of energy between the system and the surroundings. To explain the phenomena we shall take a system at equilibrium with its surroundings. Hence, the pressure P and temperature T of both the system as well as the surroundings too. Now, to disturb the equilibrium condition of the system we must change either the pressure or the temperature of the system. Suppose we take a cylinder-piston assembly, whose temperature is T and pressure is P. Now suppose, we inject a small amount of energy very slowly into the system, can you tell, what type of change we should expect in this case.

                                   Suppose we change the pressure from (P) to (P + dP) where (dP) is the change of pressure of the system, where as the pressure of the surroundings remains at (P). Then there exists a pressure difference of the flexible wall that separates our system from its surroundings. As a result a force will act on the flexible wall of the system, and the wall will move along the net force on it. Therefore, an amount of work done will be there due to the displacement of the boundary wall. There may be two type of cases, when (dP) is positive, the system does work on the surrounding as the volume of the system increases. As the volume increases from V to (V + dV) the pressure would drop to (P) from (P + dP). Hence due to this energy transfer from the system to surrounding again Equilibrium will be achieved.


VARIABLES IN THERMODYNAMICS

STATE AND COMPOSITION OF MATTER :

                                    From our common sense we can say that matters are composed of mass, a fundamental form of energy. From our early experimentation with mass and nature, we could conclude a concept of mass as a continuous physical quantity, it implies that we can divide any quantity of mass, whatever small it may be. This view is essentially evolved on the basis of our macro world perception.

                                    But within few years rapid growth of modern science shows that our perception of a continuous character of mass is an incorrect idea. Hence particle character was bestowed on mass that tells us that masses are made of tiny particles, that can independently exist in a stable condition and nicely named as molecules which are different for different materials. But it is not the fundamental particles of mass. There are more to come!

                                    So, a piece of matter is really made of very large numbers of stable molecules, which scientists conclude is made of atoms. Again atoms are composed of very tiny fundamental negatively charged particles named electrons, and the core of the atoms are called as nucleus is made of chargeless neutrons and positively charged protons.

                                    So mass is a discontinuous physical quantity and microscopic by nature! But our common perception says that it is a continuum and hence macroscopic by nature. Accordingly, there are two ways to learn thermodynamics, one is macroscopic approach, also known as Classical

                                    Thermodynamics. and the other was named as Statistical Thermodynamics. It is basically Energy Dynamics at microscopic level.


 ENERGY

                                    The focus of Thermodynamics: As the name suggests, is primarily on energy, more specifically heat energy and related variable.(Thermos means Heat energy and Temperature).

                                     So, first thermodynamic property is Energy itself! We use the term so frequently that we never think about its proper definition and understanding. Let me ask you one thing when someone mentions that he or she is feeling more energetic, what does he actually want to mean? In simple terms we can specify Energy as "something" that has the capacity to do work. Therefore, we can say that Energy has the capacity to do work, whatever it may be the change of anything is some way or other is connected with the exchange of Energy between bodies.


STORED ENERGY AND ENERGY IN TRANSITION :

                                     We have defined thermodynamics as the knowledge of Energy and its movement in the space, including the dynamics of the involved mechanisms and processes. So, our prime interest would be Energy here, hence Energy must be defined as a physical quantity (hence can be measured), which has the capacity to perform useful work against any resistance.

Here, the definition of work must be given, as thermodynamic work is different from mechanical work.


MECHANICAL WORK Vs. THERMODYNAMIC WORK:

                                     Classical or Newtonian Mechanics defines Work done as in a purely mechanical way. (a mechanical way means a macrobody having displacements). Whenever a body having a mass undergoes a displacement under the influence of a force on it, classical mechanics says a work done is there.

                                     So if F is a force vector acting on a particle due to which the particle moves travelling a "displacement" d which is also a vector, then the total work done by the force on the particle would be "dot product" of the vectors "F" and "d". So, mathematically Workdone, W can be expressed as W=F.d and in terms of "scalar" magnitude and
W=Fd CosΦ where Φ= Angle between F and d.


THERMODYNAMIC WORK:

                                     The Energy In Transition: Energy is a physical quantity and it can move from one system to another system, from one place to another place. How does energy crosses the boundary of a system? From where energy knows the direction of travel? Those are some questions which scientists want to deliver an elusive but convincing answer.

                                     So, in thermodynamics, energy will flow either as radiation (heat) or as Workdone otherwise. Hence thermodynamic work has a large domain in which mechanical work is a sub domain.


TOTAL ENERGY CONTENT OF AN AMOUNT OF GAS ENCLOSED IN A VESSEL

                                     Suppose we have an enclosed vessel, where we have kept certain amount of gas. The molecules of the gas possess energy due to the molecular vibrations of the gas molecules due to Brownian Motion. Energy, thus stored as kinetic energy of the gas molecules directly depends upon the temperature of the body. For a perfect gas the kinetic energy of the molecules, energy of a molecule directly depends upon its temperature. This energy is termed as Internal Energy. It is denoted by U. Where as internal energy per unit mass is named as Specific Internal Energy and denoted by (u) Or we can write
U=m.u where m= mass of the working substance. And if Cv is the specific heat at constant volume. Now we can write, dU = m.Cv.(dt), where as the dt is the elementary change in the temperature. But, in addition to this internal energy, there is one more type of energy. To gather all the molecules of the gas from infinity distance to enclose them at the pressure P and volume V needs workdone on the molecules, this workdone is stored in the molecules as Flow Energy and is equal to PV, hence total energy possessed by the gas molecules will be the sum of internal energy and flow work, and it is called as Enthalpy denoted by H.

H = U + PV
or
h = u + Pv (in terms of specific properties)


INEXACT DIFFERENTIALS AND EXACT  DIFFERENTIALS:

                                     In thermodynamics, an inexact differential or imperfect differential is any quantity, particularly heat Q and work W, that are not state functions (a property of a system that depends only on the current state of the system, not on the way in which the system acquired that state), in that their values depend on how the process is performed. The symbol ,₫ or δ (in the modern sense), which originated from the work of German mathematician Carl Gottfried Neumann in his 1875 Vorlesungen über die mechanische Theorie der Wärme, indicates that Q and W are path dependent. In terms of infinitesimal quantities, the first law of thermodynamics is thus expressed as:

δQ = dU + δW

where δQ and δW are inexact (path-dependent), and dU is exact (path-independent).


For an exact differential df, An inexact differential is one whose integral is path dependent. This may be expressed mathematically for a function of two variables as






                                     A differential dQ that is not exact is said to be integrable when there is a function 1/τ such that the new differential dQ/τ is exact. The function 1/τ is called the integrating factor, τ being the integrating denominator.

                                     As an example, the use of the inexact differential in thermodynamics is a way to mathematically quantify functions that are not state functions and are thus path dependent. In thermodynamic calculations, the use of the symbol ΔQ for heat is a mistake, since heat is not a state function having initial and final values. It would, however, be correct to use lower case δQ in the inexact differential expression for heat. The offending Δ belongs further down in the Thermodynamics section in the equation , which should be (Baierlein, p. 10, equation 1.11, though he denotes internal energy by E in place of U).[3] Continuing with the same instance of ΔQ, for example, removing the Δ, the equation
is true for constant pressure.


LAWS OF THERMODYNAMICS

                                    Temperature; a vital characteristics of stored energy in molecules. In a sense we can say the effect of energy stored in a molecule is the temperature of the molecule. In classical thermodynamics, temperature of a gas is nothing but the average kinetic energy of a molecule. In fact thermodynamics is the subject which deals with Energy, Equilibrium, Entropy often described as the study of  "EEE". "Molecular Motion" is the theme of thermodynamics.

                                    Thermodynamics is nothing but the energy mechanics ie the movement of energy in the space and time. It is quite evident from the name of the subject. "Thermos" is heat related to temperature and "dynamics" is the motion of it. The manifestation of energy trapped within a body is nothing but the temperature.

                                     I was an observer of nature. The smallest of smalls are the components of the nature too. I still remember the day I first time saw a thermometer, I was badly attacked by viral fever. I remember my aunt told me to clasp a thin pipe of glass, with a glittering substance inside sandwiched by inner side of my left arm and the arm pit. When I asked about the object I was told that it was an instrument, that the instrument measures the magnitude of hotness or coldness and named as "thermometer".

                                    The question that immediately popped up in my mind is that how does it measure the hotness of any object. I asked my teachers at the school, but nothing new had come out, but one thing was common in their reply to my queries and it was that whenever we place an object inside a fire, the object becomes hotter and hotter as temperature would rise and we can measure it as it would produce a rise in mercury columns.

                                    I came to know the exact answer to my queries when I read thermodynamics in the 11th Standard. when I read about kinetic theory of gases, where temperature was defined by the average magnitude of the kinetic energy of the molecules due to their non stop & compulsory motions which was analyzed by Albert Einstein and the phenomenon is called "Brownian Motion".

                                   When we touch a hot body, we feel the temperature as the molecules would transfer kinetic energy to my finger and the energy was converted into heat energy. So "Temperature" of a body is a macroscopic property of the body as a manifestation of energy contained in the whole body and which arises due to continuous bombardment of molecules with a high kinetic energy and transfer a portion of that energy to the body which is converted to heat.

                                   But it must not be the complete explanation as in solids there would not be any 'Brownian Motion' unlike the molecules of a fluid, but despite this solid still have a temperature. What is the reason of this temperature? Is it still molecular kinetic energy due to which solid posses temperature?

                                   In solid molecules are fixed at lattice points, a molecule needs a large amount of energy to make itself free from the shackles of lattice. But molecules still posses energy as it can still vibrate about its mean point ie. lattice point. This vibrational energy is responsible for solid's temperature.


Friday 29 May 2009

MULTIPLE CHOICE QUESTIONS: ENGINEERING MECHANICS

Choose the correct answer:

Q.1) In a simply supported beam of length L, a UDL of w kN/m acts on the entire span of the beam. The maximum bending moment will be
a. (w.L2)/8 b. (w.L3)/8 c. (w.L2)/4 d. (w.L3)/4

Q.2) If two forces are acting on a particle and the particle is in a stable equilibrium, then the forces are,
a. equal to each other
b. equal but opposite in direction
c. they are unequal but the direction is same.
d. none of the above.

Q.3) The example of Statically indeterminate structures are,
a. continuous beam,
b. cantilever beam,
c. over-hanging beam,
d. both cantilever and fixed beam.

Q.4) A redundant truss is defined by the truss satisfying the equation,
a. m = 2j - 3,
b. m < 2j + 3,
c. m > 2j - 3,
d. m > 2j + 3

Q.5) The property of a material to withstand a sudden impact or shock is called,
a. hardness b. ductility,
c. toughness, d. elasticity
of the material.

Q.6) The stress genarated by a dynamic loading is approximately _____ times of the stress developed by the gradually applying the same load.

Q.7) The ratio between the volumetric stress to the volumetric strain is called as
a. young's modulus
b. modulus of elasticity
c. rigidity modulus,
d. bulk modulus.

Q.8) In a Cantilever beam, the maximum bending moment is induced at
a. at the free end
b. at the fixed end
c. at the mid span of the beam
d. none of the above.

Q.9) The forces which meet at a point are called
a. collinear forces
b. concurrent forces
c. coplanar forces
d. parallel forces.

Q.10) The coefficients of friction depends upon
a. nature of the surface
b. shape of the surface
c. area of the contact surface
d. weight of the body.

Q.11) The variation of shear force due to a triangular load on simply supported beam is
a. uniform b. linear
c. parabolic d. cubic.

Q.12) A body is on the point of sliding down an inclined plane under its own weight. If the inclination of the plane is 30 degree, then the coefficient of friction between the planes will be
a. (1/3)½ b. 3½ c. 1 d. 0

Wednesday 14 January 2009

CARBURETTOR AND THE PROCESS OF CARBURETION

 

CARBURETOR                                                                                  Subhankar Karmakar

DEFINITION: A carburetor is a device that mixes air and fuel in the correct proportion for combustion in an internal combustion engine. The process of mixing air and fuel in a carburetor is known as carburetion.


STRUCTURE: The carburetor has a narrow opening called the throttle, which controls the amount of air that enters the engine. When the throttle is opened, air is drawn into the carburetor and mixed with fuel. The amount of fuel that is mixed with the air is controlled by a valve called the fuel valve, which regulates the flow of fuel into the carburetor.

 

Once the air and fuel are mixed, the resulting mixture is drawn into the engine through the intake manifold. The fuel and air mixture is then ignited by a spark plug, which causes the fuel to burn and produce energy. This energy is used to power the engine and propel the vehicle.

 

The carburetor must be adjusted to ensure that the fuel and air mixture is correct for the specific engine and driving conditions. If the mixture is too lean (too much air and not enough fuel), the engine will run poorly and may even overheat. If the mixture is too rich (too much fuel and not enough air), the engine may run rough and produce excessive emissions.

 

Carburetors were commonly used in older cars, but they have been largely replaced by fuel injection systems in modern vehicles. However, they are still used in some small engines, such as those found in lawnmowers and chainsaws.

 

CARBURETOR IN PETROL ENGINE:

 

A carburetor is a device that mixes air and fuel in the correct ratio before it enters the engine's combustion chamber. It was commonly used in older petrol (gasoline) engines before the advent of electronic fuel injection systems.

 

The basic principle of operation of a carburetor is that it uses a venturi, a narrow section of the carburetor through which air is forced to flow at high speed. As the air moves through the venturi, it creates a vacuum that draws fuel into the airflow, which mixes with the air and forms a combustible mixture.

 

The carburetor consists of several components, including a throttle valve, a choke, an idle speed adjustment screw, and a fuel bowl. The throttle valve controls the amount of air entering the engine, while the choke is used to enrich the air-fuel mixture when starting the engine. The idle speed adjustment screw regulates the engine's idle speed, while the fuel bowl stores the fuel that is drawn into the carburetor.

 

While modern petrol engines typically use electronic fuel injection systems, carburetors are still used in some older engines, as well as in small engines such as those used in lawnmowers, chainsaws, and other small equipment.

 

CARBURETOR IN DIESEL ENGINE:

 

A carburetor is a device used in gasoline engines to mix air and fuel in the correct proportions before it enters the engine cylinders for combustion.

 

However, diesel engines do not use carburetors. Instead, they use a fuel injection system, which injects fuel directly into the combustion chamber at the appropriate time, under high pressure.

 

In a diesel engine, air is compressed in the cylinder, causing it to heat up. When the air is hot enough, fuel is injected into the combustion chamber, where it ignites spontaneously due to the high temperature and pressure, without the need for a spark plug.

 

The fuel injection system in a diesel engine is more complex than a carburetor and requires precise control over the amount and timing of fuel injection to optimize combustion efficiency and reduce emissions.

COMPONENTS OF A CARBURETOR:

Carburetor in Petrol (Gasoline) Engine:

A carburetor is a crucial component in older petrol engines, responsible for mixing air and fuel in the correct ratio before it enters the engine's combustion chamber. Here's a more detailed breakdown of its components and operation:

  1. Venturi Principle: The core principle behind a carburetor's function is the Venturi effect. A venturi is a narrow section within the carburetor where air is forced to flow at high speeds. As air passes through the venturi, it accelerates, creating a region of low pressure. This low-pressure area effectively "sucks" fuel from a reservoir into the air stream.
  2. Throttle Valve: The throttle valve, also known as the butterfly valve, controls the amount of air entering the engine. When you press the accelerator pedal, it opens the throttle valve wider, allowing more air to pass through, and vice versa.
  3. Choke: The choke is a mechanism used to enrich the air-fuel mixture when starting a cold engine. By restricting the airflow, it increases the fuel-to-air ratio, making it easier for the engine to start in cold conditions.
  4. Idle Speed Adjustment Screw: This screw allows adjustment of the engine's idle speed. By controlling the amount of air allowed to bypass the closed throttle valve, it regulates the engine's speed when it's not under load.
  5. Fuel Bowl: The fuel bowl is a reservoir that stores fuel. Fuel is drawn from the bowl into the venturi as needed to maintain the correct air-fuel mixture.

Carburetor in Diesel Engine:

Diesel engines operate differently from petrol engines, and they do not use carburetors. Instead, they employ a fuel injection system, which works as follows:

  1. Compression Ignition: Diesel engines rely on high compression ratios to generate the heat needed for ignition. As air is compressed within the cylinder, its temperature increases significantly. When the piston reaches the top of its compression stroke, fuel is directly injected into the hot, highly compressed air.
  2. Fuel Injection System: Diesel fuel injection systems are highly precise and operate under high pressure. They consist of injectors that spray a fine mist of diesel fuel directly into the combustion chamber at the precise moment required for ignition. The injection timing and quantity are controlled electronically or mechanically for optimal efficiency and emissions control.
  3. No Spark Plugs: Unlike petrol engines, diesel engines do not require spark plugs because the high temperature and pressure in the cylinder are sufficient to ignite the fuel without the need for an external spark.

While carburetors were widely used in older petrol engines, diesel engines operate on a different principle altogether, using fuel injection systems to introduce fuel directly into the combustion chamber. Modern petrol engines have also largely transitioned to electronic fuel injection systems due to their efficiency and emissions control advantages. Carburetors are still found in some older engines and small equipment, but they are becoming increasingly rare in automotive applications.

 



Sunday 9 November 2008

S.F.D. for CANTILEVER BEAMS

SHEAR FORCE DIAGRAMS OF THREE DIFFERENT TYPES OF CANTILEVER LOADING





CANTILEVER BEAM

This is the most common beam in our surroundings. It is supported at one end with Fixed Joint and is known as Fixed End. The other end remains without any support and known as Free End. At the fixed end, there are a vertical reaction (RV), a horizontal reaction (RH) and a reaction moment (MR).

How To Draw the Shear Force Diagram of a Cantilever.

(i) replace the fixed joint by a vertical, a horizontal reaction force and a reaction moment.

(ii) then divide the beam into different segment depending upon the position of the loads on the beam.

(iii) take the left most segment of the beam and draw a movable section within the segment.

(iv) let the distance of the extreme left end of the beam from the movable section line be X

(v) let the upward (vertical) forces or reactions are positive and the downward forces are negative. Now the sum of the total vertical forces left to the section line is equal to the shear force at the section line at a distance X from the left most end of the beam.

(vi) as positive SF produces positive Bending Moment, hence if we multiply all the forces those are in the left side of the section line with the distances of each force from the section line added with concentrated moment (clockwise as +ve, anti-clockwise as -ve) we get bending moment. So the sum of the products of each force that is in the left side of the section with the distance of it from section line added with pure moment on this section is equal to the Bending Moment at the section line.

CANTI-LEVER BEAM

 

Draw shear force & bending moment diagrams and equations

 


Solution: At first we shall find the reaction of the canti-lever beam.
A canti-lever beam is a common type of beam which is supported on a single fixed joint at one end. A fixed joint can provide a horizontal reaction, a vertical reaction and a reaction moment. While finding reaction we should transform a distributive load (UDL, UVL) to their equivalent concentrated or point load. An equivalent load of a distributed load can be found by placing the total load at the centroid of the distributed load diagram.  


FREE BODY DIAGRAM (FBD) OF THE BEAM

SF and BM Equations:


 Section AB (0 ≤ X≤ 2)

SF = RA = 130 kN

BM = ‒ MR + RAX = ‒ 720 + 130X kN.m

At X = 0; SF = 130 kN and BM = ‒ 720 kN.m

At X =2; SF = 130 kN and BM = ‒ 720 + 260 = ‒ 460 kN.m


Section BD (2≤ X≤ 6)

SF = RA ‒  20(X‒2) = 130  ‒  20(X‒2)

BM = ‒ MR + RAX    {20(X‒2)²}/2

= ‒ 720 + 130X ‒  {20(X‒2)²}/2

 At X = 2;  SF = 130 kN and BM = ‒ 460 kN.m

At X = 6; SF = 130 ‒  80 = 50 kN and BM = ‒ 720 + 780 ‒ 160 = ‒ 100 kN.m

When a distributive load remains fully on the left side of the section line as it is in the above diagram, we should use an equivalent point load in the place of Distributive load of UVL and UDL.





Section DE (6≤ X≤ 8)

SF = RA   80 = 130    80 = 50 kN

BM = ‒ MR + RAX    80(X ‒ 4) = ‒ 720 + 130X ‒  80(X ‒ 4)

At X = 6; SF = 130   80 = 50 kN and BM = ‒ 720 + 780 ‒ 160 = ‒ 100 kN.m

At X = 8; SF = 130   80 = 50 kN and BM = ‒ 720 + 1040 ‒ 320 = 0 kN.m

SFD and BMD 

 

IC ENGINES AND COMBUSTION CHAMBER

IC ENGINES :
IC engines, or internal combustion engines, are engines in which combustion of fuel and air occurs within the engine cylinder, converting the chemical energy of the fuel into mechanical energy to perform work. The combustion chamber is a critical component of an IC engine, as it is the location where combustion occurs.

COMBUSTION CHAMBER:
The combustion chamber is typically located at the top of the cylinder in a reciprocating engine, or in the center of the combustion chamber in a rotary engine. It is designed to confine the fuel and air mixture to a small volume, allowing for efficient and controlled combustion.

The shape and size of the combustion chamber can have a significant impact on the performance and efficiency of the engine. The shape of the combustion chamber can affect the way that the fuel and air mixture is mixed and ignited, as well as the speed at which the flame front propagates through the mixture. The size of the combustion chamber can affect the compression ratio of the engine, which in turn affects the power output and fuel efficiency of the engine.

There are various types of combustion chambers used in IC engines, including the traditional spark ignition chamber and the compression ignition chamber. The spark ignition chamber is typically used in gasoline engines, where a spark plug is used to ignite the fuel and air mixture. The compression ignition chamber is typically used in diesel engines, where the fuel is ignited by the heat generated by compressing the air in the cylinder.

Overall, the design of the combustion chamber is a critical factor in the performance and efficiency of an IC engine, and careful attention must be paid to its design in order to optimize engine performance.



COMPONENTS OF A COMBUSTION CHAMBER:

The combustion chamber in an internal combustion engine is typically composed of several key components that work together to promote efficient combustion of the fuel and air mixture. The following are some of the common components of a combustion chamber:
  • Cylinder Head:
The cylinder head is the top part of the engine cylinder that contains the combustion chamber. It is typically bolted onto the engine block and is responsible for sealing the combustion chamber and providing a mounting point for the valves, spark plugs, and fuel injectors.
  • Piston:
The piston is a cylindrical component that moves up and down within the engine cylinder. It is responsible for compressing the air/fuel mixture and transmitting the force generated by combustion to the crankshaft.
  • Valves:
The valves are located in the cylinder head and are responsible for controlling the flow of air and fuel into the combustion chamber and the flow of exhaust gases out of the engine. There are typically two types of valves: intake valves and exhaust valves.
  • Spark Plug:
The spark plug is a small device that is used to ignite the fuel and air mixture in the combustion chamber. It generates an electrical spark that ignites the mixture and initiates the combustion process.
  • Fuel Injector:
The fuel injector is responsible for delivering fuel into the combustion chamber in a precise and controlled manner. It typically uses a high-pressure fuel system to inject fuel into the combustion chamber at the correct time and in the correct amount.
  • Combustion Chamber Walls:
The walls of the combustion chamber are typically made of high-strength materials such as steel or aluminum. They are designed to withstand the high temperatures and pressures generated by combustion and to provide a seal for the combustion gases.
  • Intake and Exhaust Ports:
The intake and exhaust ports are openings in the cylinder head that allow air and fuel to enter the combustion chamber and exhaust gases to exit the engine. Overall, the components of a combustion chamber work together to promote efficient and controlled combustion of the fuel and air mixture, maximizing engine performance and efficiency.

DESIGNING CRITERIA OF A COMBUSTION CHAMBER:

The design of a combustion chamber in an internal combustion engine is a critical factor in determining the performance, efficiency, and emissions of the engine. The following are some of the key criteria that must be considered in the design of a combustion chamber:
  • Air/Fuel Mixture:
The combustion chamber must be designed to provide proper mixing of air and fuel. This is necessary to ensure efficient combustion and minimize emissions.
  • Flame Propagation:
The combustion chamber must be designed to promote fast and efficient flame propagation. This is necessary to ensure that the fuel is burned completely and to maximize power output.
  • Compression Ratio:
The combustion chamber must be designed to achieve the desired compression ratio. This is important for determining the engine's power output and fuel efficiency.
  • Combustion Efficiency:
The combustion chamber must be designed to promote complete combustion of the fuel. This is necessary to minimize emissions and maximize fuel efficiency.
  • Turbulence:
The combustion chamber must be designed to promote turbulence in the air/fuel mixture. This is important for promoting efficient combustion and minimizing emissions.
  • Wall Heat Transfer:
The combustion chamber must be designed to minimize heat transfer to the cylinder walls. This is important for reducing engine heat loss and maximizing power output.
  • Knock Resistance:
The combustion chamber must be designed to resist engine knock. This is important for maximizing power output and engine efficiency.
  • Emissions:
The combustion chamber must be designed to minimize emissions of pollutants such as nitrogen oxides (NOx), carbon monoxide (CO), and particulate matter (PM). This is important for meeting emissions regulations and minimizing environmental impact. Overall, the design of the combustion chamber is a complex process that requires consideration of multiple factors. Careful attention to these criteria is necessary to optimize engine performance and meet emissions regulations.


FAILURE CRITERIA OF COMBUSTION CHAMBER:

The failure of a combustion chamber in an internal combustion engine can be catastrophic and can result in engine damage, reduced performance, or even complete engine failure. The following are some of the common failure criteria of a combustion chamber:
  • Overheating:
One of the most common failure modes of a combustion chamber is overheating. This can be caused by a variety of factors, such as a lean air/fuel mixture, excessive compression, or a malfunctioning cooling system. Overheating can cause cracking or warping of the combustion chamber, leading to leaks or even catastrophic failure.
  • Detonation:
Detonation occurs when the fuel/air mixture in the combustion chamber detonates spontaneously instead of burning in a controlled manner. This can be caused by factors such as excessive compression, hot spots in the combustion chamber, or low-quality fuel. Detonation can cause the combustion chamber to deform or crack, leading to reduced engine performance or even complete engine failure.

  • Pre-ignition:
Pre-ignition occurs when the fuel in the combustion chamber ignites before the spark plug fires. This can be caused by factors such as hot spots in the combustion chamber, high compression, or low-quality fuel. Pre-ignition can cause damage to the combustion chamber and other engine components, leading to reduced engine performance or even complete engine failure.
  • Corrosion:
Corrosion can occur in the combustion chamber due to the corrosive nature of the fuel or the combustion process itself. Corrosion can weaken the walls of the combustion chamber, leading to cracks or other types of damage that can compromise engine performance.
  • Mechanical Damage:
Mechanical damage to the combustion chamber can occur due to improper installation, poor maintenance, or external factors such as debris striking the engine. This type of damage can cause leaks or other types of damage that can affect engine performance or even cause complete engine failure. Overall, the failure of a combustion chamber can have severe consequences for engine performance and reliability. Regular maintenance and proper operation of the engine can help to prevent these failure modes and ensure the long-term reliability and performance of the engine.