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116   Analysis and Design of Energy Geostructures


                magnitude of the shear stresses at the surface wall, τ s . This relationship is usually
                expressed through the local friction coefficient of the surface:

                                                 C f    τ s                           ð3:48Þ
                                                      ρ f v N
                                                        2
                   For Newtonian fluids, that is fluids for which the viscous stresses arising from their
                flow are linearly proportional to the local strain rate at every point, the surface shear
                stress can be determined through Newton’s law as

                                                τ 5 μ  dv rf ;i                       ð3:49Þ
                                                     f  dn i
                   With regards to the problem depicted in Fig. 3.20A, the surface shear stress can
                thus be determined as

                                               τ s 5 μ  dv x                          ð3:50Þ
                                                         y50
                                                    f
                                                      dy
                   The development of the thermal boundary layer is a consequence of the presence
                of a temperature difference between the surface and the free stream (cf. Fig. 3.20B).
                Due to the presence of such a temperature difference, the fluid temperature is equal
                to the surface temperature at the wall in the boundary layer, varies within the bound-
                ary layer and remains constant at a temperature outside the boundary layer that is
                usually termed the free stream temperature, T N . The thickness of the thermal
                boundary layer, δ th , is usually considered to correspond to a fluid temperature of
                T δ 5 ðT s 2 TÞ=ðT s 2 T N Þ 5 0:99. The significance of the thermal boundary layer
                thus depends on the magnitude of difference between the temperature at the surface
                wall, T s , and the temperature of the free stream, T N . This relationship is usually
                expressed through the local convection heat transfer coefficient, h c , which can be
                determined by considering that at the surface wall heat transfer occurs by conduction
                only (i.e. Fourier’s law can be applied to the fluid) and convection governs heat trans-
                fer in the fluid in motion (i.e. Newton’s law of cooling can be used). With regards to
                the problem depicted in Fig. 3.20B, Fourier’s law reads


                                                 52 λ  @T
                                             _ q          j y50                       ð3:51Þ
                                              cond
                                                        @y
                and can be substituted into Newton’s law of cooling to yield the convection heat
                transfer coefficient

                                                   2 λ  @T  j
                                              h c 5    @y y50                         ð3:52Þ
                                                    T s 2 T N
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