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Chapter 1 heat trasfer

Apr 03, 2018

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    Chapter 1: Introduction and

    Basic Concepts

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    ObjectivesWhen you finish studying this chapter, you should be able to:

    Understand how thermodynamics and heat transfer are related toeach other,

    Distinguish thermal energy from other forms of energy, and heattransfer from other forms of energy transfer,

    Perform general energy balances as well as surface energy

    balances, Understand the basic mechanisms of heat transfer, which are

    conduction, convection, and radiation, and Fourier's law of heatconduction, Newton's law of cooling, and the StefanBoltzmannlaw of radiation,

    Identify the mechanisms of heat transfer that occur simultaneouslyin practice,

    Develop an awareness of the cost associated with heat losses, and

    Solve various heat transfer problems encountered in practice.

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    Thermodynamics and Heat Transfer

    The science ofthermodynamics deals with theamount of heat transferas a system undergoes aprocess from one equilibrium state to another,

    and makes no reference to how long the processwill take.

    The science ofheat transfer deals

    with the determination of the rates

    of energy that can be transferred

    from one system to another as a

    result of temperature difference.

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    Thermodynamics deals with equilibrium statesand changes from one equilibrium state toanother. Heat transfer, on the other hand, deals

    with systems that lack thermal equilibrium, andthus it is a nonequilibrium phenomenon.

    Therefore, the study of heat transfer cannot bebased on the principles of thermodynamics alone.

    However, the laws of thermodynamics lay theframework for the science of heat transfer.

    Thermodynamics and Heat Transfer

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    Heat Transfer

    The basic requirement for heat transferis the presence

    of a temperature difference.

    The second law requires that heat

    be transferred in the direction of

    decreasing temperature. The temperature difference is the driving force for heat

    transfer.

    The rate ofheat transferin a certain direction depends

    on the magnitude of the temperature gradient in thatdirection.

    The largerthe temperaturegradient, the higherthe rateofheat transfer.

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    Application Areas of Heat Transfer

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    Heat and Other Forms of Energy

    Energy can exist in numerous forms such as: thermal,

    mechanical,

    kinetic,

    potential,

    electrical,

    magnetic,

    chemical, and

    nuclear.

    Their sum constitutes the total energyE(oreon aunit mass basis) of a system.

    The sum of all microscopic forms of energy is calledthe internal energyof a system.

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    Internal energy may be viewed as the sum ofthe kinetic and potential energies of themolecules.

    The kinetic energy of the molecules is calledsensible heat.

    The internal energy associated with thephase of

    a system is called latent heat.

    The internal energy associated with the atomicbonds in a molecule is called chemical(or

    bond) energy. The internal energy associated with thebonds

    within the nucleus of the atom itself is callednuclear energy.

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    Internal Energy and Enthalpy

    In the analysis of systemsthat involve fluid flow,we frequently encounterthe combination of

    properties u andPv.

    The combination isdefined as enthalpy(h=u+Pv).

    The termPv representsthe flow energy of thefluid (also called the flowwork).

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    Specific Heats of Gases, Liquids, and

    Solids Specific heatis defined as the energy required to

    raise the temperature of a unit mass of a substance byone degree.

    Two kinds of specific heats: specific heat at constant volumecv, and specific heat at constant pressurecp.

    The specific heats of a substance, in general, dependon two independent properties such as temperature

    and pressure. For an ideal gas, however, they depend on

    temperature only.

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    Specific Heats

    At low pressures all real gases approach ideal gasbehavior, and therefore their specific heats depend ontemperature only.

    A substance whose specific volume (or density) does

    not change with pressure is called an incompressiblesubstance.

    The constant-volume and constant-pressure specificheats are identical for incompressible

    substances. The specific heats of incompressible

    substances depend on temperature

    only.

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    Energy Transfer

    Energy can be transferred to or from a given mass by two

    mechanisms: heat transfer, and

    work.

    The amount of heat transferred during a process is denoted by Q.

    The amount of heat transferred per unit time is called heattransfer rate, and is denoted by Q.

    The total amount of heat transferQduring a time interval Dtcanbe determined from

    The rate of heat transfer per unit area normal to the direction ofheat transfer is called heat flux, and the average heat flux isexpressed as

    0

    (J)

    t

    Q Qdt

    D

    2

    (W/m )

    Q

    q A

    (1-6)

    (1-8)

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    The First Law of Thermodynamics

    The first law of thermodynamics states that energycan neither be created nor destroyed during a process;

    it can only change forms.

    The energy balancefor any system undergoing any

    process can be expressed as (in the rate form)

    Total energy

    entering the

    system

    Total energy

    leaving the

    system

    Change in the

    total energy of

    the system

    - =

    (W)in out systemE E dE dt

    Rate of net energy transfer

    by heat, work, and mass

    Rate of change in internal

    kinetic, potential, etc., energies

    (1-9)

    (1-11)

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    In heat transfer problems it is convenient to write

    a heat balanceand to treat the conversion ofnuclear, chemical, mechanical, and electrical

    energies into thermal energy as heat generation.

    The energy balance in that case can be expressedas

    , (J)in out gen thermal systemQ Q E E D

    Net heat

    transfer

    Change in

    thermal energy

    of the system

    Heat

    generation

    (1-13)

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    Energy Balance

    Closed systems

    Stationary closed

    system, no work:

    Steady-Flow Systems

    For system with one inlet and

    one exit:

    When kinetic and potentialenergies are negligible, and

    there is no work interaction

    (J)vQ mc T D (kg/s)in out m m m

    (kJ/s)pQ m h mc T D D

    (1-15)

    (1-18)

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    Heat Transfer Mechanisms

    Heat can be transferred in three basic modes: conduction,

    convection,

    radiation.

    All modes of heat

    transfer require the

    existence of a temperature difference.

    All modes are from the high-temperature

    medium to a lower-temperature one.

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    Conduction Conduction is the transfer of energy from the more

    energetic particles of a substance to the adjacent lessenergetic ones as a result of interactions between the

    particles.

    Conduction can take place in solids,

    liquids, or gases

    In gases and liquids conduction is due to

    the collisions and diffusion of the

    molecules during their random motion.

    In solids conduction is due to the

    combination ofvibrations of the

    molecules in a lattice and the energy

    transport by free electrons.

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    Conduction

    1 2 (W)condT T T

    Q kA kAx x

    D

    D D

    Area Temperature differenceRate of heat conductionThickness

    where the constant of proportionality kis the

    thermal conductivityof the material.

    In differential form

    which is called Fouriers law of heat conduction.

    (1-21)

    (1-22)(W)conddT

    Q kAdx

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    Thermal Conductivity

    The thermal conductivity of a material is a

    measure of the ability of the material to conduct

    heat.

    High value for thermal conductivity

    good heat conductor

    Low valuepoor heat conductororinsulator.

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    Thermal Conductivities of Materials

    The thermal conductivities

    ofgases such as air vary by

    a factor of104 from those

    ofpure metals such ascopper.

    Pure crystals and metals

    have the highest thermal

    conductivities, and gasesand insulating materials the

    lowest.

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    Thermal Conductivities and

    Temperature

    The thermal conductivities

    of materials vary with

    temperature.

    The temperaturedependence of thermal

    conductivity causes

    considerable complexity in

    conduction analysis.

    A material is normally

    assumed to be isotropic

    (i.e., uniform in alldirections .

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    Thermal diffusivity

    The thermal diffusivity represents how fast heat

    diffuses through a material.

    Appears in the transient heat conduction analysis.

    A material that has a high thermal conductivity or a

    low heat capacity will have a large thermal diffusivity. The larger the thermal diffusivity, the fasterthe

    propagation ofheat into the medium.

    2Heat conducted ( m s)Heat stored p

    k

    c

    (1-23)

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    Convection

    Convection is the mode of energy transfer between a

    solid surface and the adjacent liquid or gas that is in

    motion. Convection is commonly classified into three sub-

    modes:

    Forced convection,

    Natural (or free) convection,

    Change of phase (liquid/vapor,

    solid/liquid, etc.)

    Convection =Conduction+Advection

    (fluid motion)

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    Convection

    The rate ofconvection heat transferis expressed byNewtons law of coolingas

    his the convection heat transfer coefficientinW/m2C.

    h depends on variables such as the

    surface geometry, the nature of fluid

    motion, the properties of the fluid,

    and the bulk fluid velocity.

    ( ) (W)conv s sQ hA T T (1-24)

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    Radiation

    Radiation is the energy emitted by matter in the form ofelectromagnetic waves(orphotons) as a result of thechanges in the electronic configurations of the atoms ormolecules.

    Heat transfer by radiation does not require the presence ofan intervening medium.

    In heat transfer studies we are interested in thermalradiation (radiation emitted by bodies because of their

    temperature). Radiation is a volumetric phenomenon. However, radiation

    is usually considered to be asurface phenomenon forsolids that are opaque to thermal radiation.

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    The maximum rate of radiation that can be emitted from a

    surface at a thermodynamic temperature Ts(in K or R) is givenby the StefanBoltzmann lawas

    s=5.670X108 W/m2K4 is the StefanBoltzmann constant.

    The idealized surface that emits radiation at this maximum rate

    is called a blackbody.

    The radiation emitted by all real surfaces is less than the

    radiation emitted by a blackbody at the same temperature, and

    is expressed as

    eis the emissivityof the surface.

    4

    ,max (W)emit s sQ A Ts

    4

    ,max (W)

    0 1

    emit s sQ A Tes

    e

    Radiation - Emission

    (1-25)

    (1-26)

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    Radiation - Absorption

    The fraction of the

    radiation energy incident

    on a surface that is

    absorbed by the surface istermed the absorptivity .

    Both eand of a surface depend on the temperatureand the wavelength of the radiation.

    0 1