Page 66 - Introduction to Computational Fluid Dynamics
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                        2.9 PROBLEMS FROM RELATED FIELDS
                        slope of the temperature profile at the point of discontinuity (x = 0.0125 m) in 10:49  45
                        conductivity. Finally, by assigning different values to k 2 , k 3 , r 2 , r 3 , and t, it would
                        be possible to carry out a parametric study to aid optimisation of fin volume and
                        economic cost in a separate design study.
                        2.9 Problems from Related Fields
                        Quite a few problems from the fields of fluid mechanics, convective heat transfer,
                        and diffusion mass transfer are governed by equations that bear similarity with
                        Equation 2.5. Only the dependent variable, the coefficients, and the source term
                        need to be interpreted appropriately. We discuss such problems next.


                        Fully Developed Laminar Flow
                        Steady, fully developed laminar flow in a tube is governed by
                                              ∂         ∂u         dp
                                                  µ2π r      − 2π r    = 0,                (2.77)
                                             ∂r         ∂r          dz
                        where u is velocity parallel to the tube axis and the pressure gradient is a negative
                        constant. Since velocity u is directed in the z direction, it can be treated as a scalar
                        with respect to the r direction. Comparison with Equation 2.5 shows that T ≡ u,

                        ∂x ≡ ∂r, A ≡ 2πr, k ≡ µ, andq ≡−dp/dz. For a circular tube, u = 0atr = R
                        (tube radius) and ∂u/∂r = 0 at the tube axis r = 0. Equation 2.77 is also applicable
                        to an annulus with boundary conditions u = 0at r = R i and r = R o . Similarly, the
                        equation is applicable to flow between parallel plates if we set A = 2π r = 1 and
                        ∂x ≡ ∂r ≡ ∂y, where y is measured from the symmetry axis.

                        Fully Developed Turbulent Flow
                        In this case, if Boussinesq approximation is considered valid then the axial velocity
                        is governed by
                                           ∂               ∂u  
       dp
                                               (µ + µ t )2π r   − 2π r     = 0,            (2.78)
                                          ∂r               ∂r          dz


                        where the turbulent viscosity µ t = ρ l  2   ∂u    with
                                                          m  ∂r
                                                           y                y

                                         ⎧                  +
                                         ⎪ κ y 1 − exp −             for       < y l ,
                                         ⎪
                                                           26               R
                                         ⎨
                                     l m =                                                 (2.79)
                                                              y
                                         ⎪
                                         ⎪
                                         ⎩ 0.085 R     for      > y l ,
                                                              R
                                                                      √
                        where κ = 0.41, y = R − r, y l 
 0.2, and y = y  τ w /ρ /ν with τ w the shear
                                                                 +
                        stress at the wall (i.e., τ w = µ∂u/∂y | y=0 ). Clearly, Equation 2.78 can be solved
                        iteratively by estimating the turbulent viscosity distribution from the velocity
                        gradient.
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