Page 179 - Fundamentals of The Finite Element Method for Heat and Fluid Flow
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TRANSIENT HEAT CONDUCTION ANALYSIS
                                                      5
                                                            2
                        is exposed to (a) a heat flux of 3 × 10 W/m and (b) a sudden rise in surface temperature
                             ◦
                        of 200 C. Calculate the temperature at a depth of 1 cm after a time of 10 seconds for both
                        cases. Verify the results with analytical results.                    171
                                                                                          ◦
                        Exercise 6.10.2 A fin of length 1 cm is initially at the ambient temperature of 30 C. If the
                        base temperature is suddenly raised to a temperature of 150 C and maintained at that value,
                                                                       ◦
                        determine the temperature distribution in the fin after 30 seconds if the thermal diffusivity
                                                   2
                        of the fin material is 1 × 10 −5  m /s. The heat transfer coefficient between the fin surface
                                              2◦
                        and the ambient is 100 W/m C. The cross section of the fin is 6 mm by 5 mm.
                        Exercise 6.10.3 A short aluminium cylinder 2.5 cm in diameter and 5 cm long is initially
                        at a uniform temperature of 100 C. It is suddenly subjected to a convection environment
                                                  ◦
                            ◦
                                             2◦
                        at 50 C and h = 400 W/m C. Calculate the temperature at a radial position of 1 cm from
                        outer surface and a distance of 0.5 cm from one end of the cylinder 10 seconds after exposure
                        to the environment.
                        Exercise 6.10.4 A plane wall of thickness 4 mm has internal heat generation of 25 MW/m 3
                        with thermal properties of k = 20 W/m C, ρ = 8000 kg/m 3  and specific heat c p =
                                                          ◦
                        500 J/kg C. It is initially at a uniform temperature of 50 C and is suddenly subjected to
                                                                       ◦
                               ◦
                        heat generation and a convective boundary condition as shown in Figure 6.17 Calculate
                        the temperature at a location of 2 mm after 10 seconds.
                        Exercise 6.10.5 A stainless steel plate size 2 cm × 1 cm is surrounded by an insulating
                                                                                         ◦
                        block as shown in Figure 6.18 and is initially at a uniform temperature of 40 C with a
                                                                                                2
                                               ◦
                        convection environment at 40 C. The plate is suddenly exposed to a radiant flux of 15 kW/m .
                        Calculate the temperature at the centre of the top and bottom surfaces after 10 s. Take the
                                                                            3
                                                                                           ◦
                        properties of the stainless steel as k = 18 W/mK, ρ = 8000 kg/m , c p = 0.46 kJ/kg C, and
                                  2
                        h = 30 W/m K.
                                                   2
                                                                            2
                                           h = 500 W/m °C           h = 400 W/m °C
                                           T a = 30°C               T a = 100°C
                                             Figure 6.17 Plane wall discretization


                                                    q rad
                                                                 h, T a

                                               1 cm



                                                             2 cm
                                               Figure 6.18 Stainless steel plate
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