Page 72 - Introduction to Computational Fluid Dynamics
P. 72

P1: IWV/ICD
                                        0 521 85326 5
                           CB908/Date
            0521853265c02
                        EXERCISES
                        Table 2.9: Properties of the wall materials.               May 25, 2005  10:49  51
                                           3
                        Material     ρ (kg/m )  C (J/kg-K)  k (W/m-K)
                        Plasterboard  1000     1380       0.15
                        Fibreglass     30       850       0.038
                        Plywood       545      1200       0.1
                                         2                         2
                                                   ∗
                            where B = (r  ∗  − 1)/lnr and A = 1 + r  ∗  − B. Hence, compare the pre-
                            dicted friction factor based on a hydraulic diameter D h = 2(R o − R i ) with
                                                             16        2
                                                           =     1 − r  ∗  .
                                                  ( fRe) D h
                                                              A
                        20. Solve Equation 2.78 for turbulent flow in a circular tube and compare your
                            results with the expressions [33]
                                          ⎧
                                                                               +
                                             +
                                          ⎪ y ,                               y ≤ 11.6
                                     u    ⎨

                                       =             1.5(1 + r/R)
                                                                               +
                                          ⎩ 2.5ln y +              + 5.5,     y > 11.6.
                                    u τ   ⎪
                                                      1 + 2(r/R) 2
                            Also compare the predicted friction factor f with f = 0.079Re −0.25  for Re <
                                                                         4
                                  4
                            2 × 10 and with f = 0.046Re −0.2  for Re > 2 × 10 . Plot the variation of total
                            (laminar plus turbulent) shear stress with radius r. Is it linear? (Hint: Make sure
                                                                  +
                            that the first node away from the wall is at y ∼ 1.)
                        21. Engine oil enters a tube (D = 1.25 cm) at uniform temperature T in = 160 C.
                                                                                             ◦
                            The oil mass flow rate is 100 kg/h and the tube wall temperature is maintained at
                            T w = 100 C.Ifthetubeis3.5mlong,calculatethebulktemperatureofoilatexit
                                     ◦
                                                                             3
                            from the tube. The properties of the oil are ρ = 823 kg/m , C p = 2,351 J/kg-K,
                                      2
                                  −5
                            ν = 10 m /s, and k = 0.134 W/m-K. Plot the axial variation of Nusselt num-
                            ber Nu x and bulk temperature T b,x and compare with the exact solution given
                            in Table 2.10.
                        Table 2.10: Thermal entry length solution – T w =
                        constant [33].
                        (x/R)/(Re Pr)     Nu x      (T w − T b )/(T w − T in )
                        0                 ∞         1.0
                        0.001            12.80      0.962
                        0.004             8.03      0.908
                        0.01              6.0       0.837
                        0.04              4.17      0.628
                        0.08              3.77      0.459
                        0.10              3.71      0.396
                        0.20              3.66      0.190
                        ∞                 3.66      0.0
   67   68   69   70   71   72   73   74   75   76   77