HEAT TRANSFER: CONDUCTION AND CONVECTION

HEAT TRANSFER: CONDUCTION AND CONVECTION

  Dr. B. Jayaraman FDP on CFD Lecture 5: 7 th June 2016,

  SoME, SASTRA University, Thanjavur OUTLINE

  • Introduction
  • ConductionConvection

   Forced ConvectionFree Convection

  • Other ModelsConclusion

  MODES OF HEAT TRANSFER

  THERMAL CHARACTERISTICS Temperature Distributions Amount of Heat Lost or gained

  Thermal Analysis Thermal Gradients Thermal Fluxes Thermal Analysis

  • + Thermal Stresses Stress Analysis

PHENOMENA (MODELS)

  • ConductionConvection

   Forced ConvectionNatural convectionBoiling (Multiphase)

  • RadiationSpecies diffusion and CombustionConjugate heat transfer
  • Periodic heat transfer

BOUNDARY CONDITIONS

  • Heat FluxTemperatureConvectionRadiationMixed – Combination of Convection and

  Radiation boundary conditions

  • Via System Coupling

  PROPERTIES

Fluid properties such as heat capacity, conductivity and viscosity

can be defined as:

   Constant  Temperature-dependent  Composition-dependent  Computed by kinetic theory  Computed by user-defined functions

  • Density can be treated as

   Constant (with optional Boussinesq modeling)  Temperature-dependent  Computed as ideal gas law  Composition-dependent  User defined functions

  OUTLINE

  • Introduction
  • Conduction
  • Convection

   Forced ConvectionFree Convection

  • Other ModelsConclusion

  CONDUCTION conducted Generated

  • + Energy Heat + = conducted Energy Internal change of Rate of into CV within CV out of CV Energy in CV

  2 2 2 c

    ρ

  T T T q T

   

p2     2 2 

   x y z k k t

  

   

 

2-DIM. PROBLEM

  

Physical domain of Slab with square cross section

T T T T

    T

  T T T

  2L

W 3 m q 2-dim, Steady state with heat generation 2 2 2 2   

       

      T k q y x T

  2-DIM,STEADY STATE TT x yGeometrically and thermally symmetric θ  ; q L L L 2 X  ; Y 2k 2 TT

      θ θ

  L

  1 2    2    XY Non-dim Boundary Conditions  

  W q     3 TT dT m At X = 0 θ

    xdXAt X = 1  θ d T At Y = 0 dY θ

   L yAt Y = 1  

  θ

Computational Domain of Slab with square cross section

  2-DIM,UNSTEADY STATE SQUARE PLATE TT x y t i α  ; X  ; Y   Infinitely long plate, initially at T Then suddenly maintained at T o i θ TT L L L o i τ 2 2 2

  2 2     

  θ θ θ      T T T 2   2

    α 2 2

     

   XY  τ

   xyt  

    Non-dim Boundary Conditions T To At  τ= 0 θ

  L  1 T T T o For At X = 1 τ> 0 d θ x At X = 0 d dX θ T  L At Y = 0 dY θ y At Y = 1 1

   θ OUTLINE

  • IntroductionConduction
  • Convection

   Forced ConvectionFree Convection

  • Other ModelsConclusion

  CONVECTION

  • Diffusion Transport + Advection Transport

  driver

  • Advecting variable(velocity) 

  passenger

  • Advected variable(temperature)

  

  • Transports Momentum and Energy

FORCED CONVECTION

  Diffusion Transport

  • Random Molecular Motion  Molecular heat-flux includes only conduction heat transfer

   Molecular momentum-flux includes both pressure and viscous forces (fluid statics/dynamics)

FORCED CONVECTION

  • Advective Transport

   Bulk or macroscopic motion of the fluid

 Such motion, in the presence of a temperature

and velocity gradient contributes to heat and momentum transfer, respectively

ENERGY BALANCE

    

  Unsteady term Conduction term = + Convection term

  • + Source term
  •   ρ ρ

       2 2 2 2 2 2

       

       

        

         

       

        

         

       

      Rate of Energy flow into CV Rate of Energy flow out of CV = + Net Viscous Work done on CV

    • + Rate of accumulation of Energy in CV

      Q y T y

        

         

       

       

       

       

        

        

       

      T c p

      T v x T u p c t

      T x T k z T w y

        

    VISCOUS WORK

      Work done by surface stresses in x-direction

    ENERGY EQUATION

      S E = PE +

    q

      Q If work done by surface stresses are included KINETIC AND INTERNAL ENERGY

    ENTHALPY EQUATION

    • An alternative form of the energy equation is the total enthalpy equation.

       Specific enthalpy h = i + p/ρ 2 2 2 = h + ½ (u +v +w ) = E + p/ ρ

      Total enthalpy h

    TRANSPORT EQUATIONS

       = pressure, three velocity components, enthalpy, temperature and density

      CONSERVATION EQUATION and associated scalar fields.

    solved by finite volume based CFD programs to calculate the flow pattern

      1-dim, STEADY CONVECTION-DIFFUSION U o

      T o dx dT dx dT U o T

    T- T

    1 > T o w Slug Flow through a long channel of length L

      2 2 x T x T

      U o  

        

      α 2 Pe  

       θ θ

      α θ L U Pe L x X T T T T o o i o   

        ; ;

    EXACT SOLUTION

      Pe

      0 and large diffusivity,

    • For small U o

       the solution is T= x (T linear in x )

      Pe>>0

    • For large U o

       Φ grows slowly with x and them suddenly rises to Φ L over a short distance close to x=L

      1 ) exp( 1 ) exp( ) ( 

        Pe Pex

      T x

    NUMERICAL SOLUTION

      In terms of Central difference Scheme (CDS)    2 Pe θ θ θ θ θ i     1 i 1 i 1 i i 1

       2 1 2 ( )X X Where Pe = Pe Δx   Pe   Pe c 2 2 θ    θ   θ  i c i 4 1 c i 1 For Pe ≥ 2 Solution shows wiggles, a computational instability c oscillation which disappears on fine grids as Pe becomes less than 2 c

      If upstream differencing is used in convection term?

    UPWIND SCHEME

        2  Pe θ θ θ θ θ i i 2  (  ) X    1 i 1 i i X 2 1 Known as First Order Upwind scheme 1   Pe    θ θ  c i   1 i 1

       θ i 2  Pe c For large Pe diffusion term is overestimated Solution is stable c

      Hence refined grid is selected at large Pe

    c

    OTHER SCHEMES

    • Quest for an optimal (stable as well as accurate)

      advection discretization procedure continues

    • Other promising alternatives are higher order

      schemes such as Second Order Upwind and QUICK

    • QUICK has been found better as compared to the

      SOU advection scheme

      FLOW IN PARALLEL PLATES T m 1. Constant heat flux Assumptions: TT s 3. Steady Flow

      2. Thermally fully developed flow h

        ucTdy T ( x ) T ( y , x )

        s ρ

       s    T m   x T ( x )  T ( y , x ) s m   m c

      

      At the plate surface ) ( ) ( ) ( ) ( ) (

    x f

    T x x T y T k T x x T q m s m s s

         

         ) (x f h cConvective heat transfer Coefficient

      FLOW IN PARALLEL PLATES

      Energy balance on CV dx x

      T c m x q m  

         

      2 FLOW IN PARALLEL PLATES FLOW IN PARALLEL PLATES

      2 2

         

         TTTTT

       

      cc uvk

       

      ρ ρ p

       

      p 2 2

         

       txyxy  

         

       

      2 2 2

              T   TTT

       

      c u   k

        

      ρ 2 2 2 p

             

       xyxy  

        2       Solving  

         TT

       

      h D c h u

       

      α 2

       8 .

      24  

         xy

       

      k

          D =2R h CIRCULAR POISEUILLE FLOW

      OUTLINE

    • IntroductionConductionConvection

       Forced Convection Free Convection

      

    • Other ModelsConclusion

    NATURAL CONVECTION

      Hot Surface Upward Cold Surface Downward

    • Hot Surface Downward Cold Surface Upward

    NATURAL CONVECTION

    • The fluid motion is induced by the heat transfer
    • Density and temperature are related; hotter gases

      rise…

    • Thermal expansion coefficient is a characteristic

      property of fluids

    • The momentum equation must be written in

      compressible form (density is varying) and includes a source term

    FREE CONVECTION

      α  

      At y = 0    T T v u ; At τ= 0 For τ> 0    T T v u ; s T T v u    ; y,v x,u

      Flow over a heated vertical flat plate Boundary conditions: Energy equation Momentum equation Continuity equation At x = 0

          y v x u

      β ν 2 2  

          T T g y u y u v x u u t u

         

          

        

        

       

       

        

         

       

        

         

       

       2 T 2 y T y v x T u t T

    FREE CONVECTION

    • The momentum and energy equations are coupled by

      via the temperature Typically called Boussinesq fluids…

    • Boussinesq Model: Model treats density as a

      

    constant value in all solved equations, except for the

    buoyancy term in the momentum equation

    • the Boussinesq approximation is valid when

      (T − T ) << 1 β

      OUTLINE

    • IntroductionConductionConvection

       Forced ConvectionFree Convection

    • Other Models
    • Conclusion
    Conjugate Heat Transfer

    • Ability to compute conduction of heat through solids,

      coupled with convective heat transfer in fluid

    • In 2D Cartesian coordinates:

      W = wall

       

        

        

         

        

      

      ∂ ∂ ∂ ∂

      ∂ ∂ ∂ ∂

      ρ ∂ ∂

    • Properties varies with location and Temperature  
    • T q y k y x

      T k x T c t w w w w Periodic Heat Transfer

      • Used when flow and heat transfer patterns are repeatedCompact heat exchangersFlow across tube banks
      • Outflow at one periodic boundary is inflow at the other
      • Geometry and boundary conditions repeat in streamwise

        direction inflow outflow

        OUTLINE

      • IntroductionConductionConvection

         Forced ConvectionFree Convection

      • Other Models
      • Conclusion

        OPTIMIZATION

      • Increasing the area A, e.g. by using profiled pipes and ribbed surfaces.
      • Increasing ΔT (which is not always controllable).
      • For conduction, increasing kf /d.
      • Increase h by not relying on natural

        convection, but introducing forced convection

        CONCLUSION

      • Thermal conditions at walls, flow boundaries and fluid properties required for energy equation.
      • • Chemical reactions, such as combustion, can lead to source terms to be included in the enthalpy equation.
      • • Analytical solutions exist for some simple problems and we must rely on computational methods to solve most industrially relevant applications.

      THANK YOU

      • • An energy equation must be solved together with