 
          2986
        
        
          Proceedings of the 18
        
        
          th
        
        
          International Conference on Soil Mechanics and Geotechnical Engineering, Paris 2013
        
        
          T
        
        
          in
        
        
          T
        
        
          out
        
        
          T
        
        
          out
        
        
          frost body
        
        
          inner pipe (PE)
        
        
          outer pipe (steel)
        
        
          refrigerant
        
        
          
            s
          
        
        
          
            Q
          
        
        
          
            e
          
        
        
          
            Q
          
        
        
          Figure 1. Freeze pipe in detail with occurring heat flow.
        
        
          The heat flow
        
        
          
            s
          
        
        
          
            Q
          
        
        
          between the soil and the outer freeze pipe
        
        
          comprises conductive heat flow through the outer freeze pipe
        
        
          and convective heat flow due to the flowing refrigerant. The
        
        
          heat flow
        
        
          
            e
          
        
        
          between the down- and upstream via the inner
        
        
          freeze pipe can be divided into two mechanisms. On the one
        
        
          hand, conductive heat flow through the inner freeze pipe and on
        
        
          the other hand convective heat flow both inside and outside the
        
        
          inner freeze pipe. In case of a flowing refrigerant the vertical
        
        
          heat transfer is dominated by advection which is already
        
        
          considered in the horizontal heat flow. Therefore the vertical
        
        
          conductive heat flow within the refrigerant is neglected.
        
        
          
        
        
          
            Q
          
        
        
          
        
        
          The heat transfer due to conduction can be determined by
        
        
          using Fourier’s law. The conductive heat flow for a coaxial
        
        
          freeze pipe for n conductive layers with the thermal
        
        
          conductivity of the pipe material
        
        
          
        
        
          i
        
        
          [W/(mK)] results in:
        
        
          
        
        
          
        
        
          
        
        
           
        
        
          
            n
          
        
        
          
            i
          
        
        
          
            i,in i,out
          
        
        
          
            i
          
        
        
          
            i
          
        
        
          
            conduction
          
        
        
          
            )r rln(
          
        
        
          
            T
          
        
        
          
            Q
          
        
        
          1
        
        
          2
        
        
          
        
        
          (2)
        
        
          The convective heat flow depends on the heat transfer
        
        
          coefficient
        
        
          
        
        
          i
        
        
          [W/(m²K)]:
        
        
          
        
        
          
        
        
            
        
        
          
            n
          
        
        
          
            i
          
        
        
          
            i i
          
        
        
          
            convection
          
        
        
          
            T r
          
        
        
          
            Q
          
        
        
          1
        
        
          2
        
        
          
        
        
          (3)
        
        
          The heat transfer coefficient depends on the freeze pipe
        
        
          geometry and the flow and material properties of the refrigerant.
        
        
          As a function of the Nusselt number Nu the heat transfer
        
        
          coefficient is defined as (Baehr and Stephan 2006):
        
        
          
            hydrauli
          
        
        
          
            F
          
        
        
          
            d
          
        
        
          
            Nu
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          (4)
        
        
          with the thermal conductivity of the refrigerant
        
        
          
        
        
          F
        
        
          and the
        
        
          hydraulic freeze pipe diameter d
        
        
          hydraulic
        
        
          . The hydraulic diameter
        
        
          of the inner freeze pipe corresponds to its inner diameter
        
        
          (see Figure 2).
        
        
          d
        
        
          in, outer pipe
        
        
          d
        
        
          in, inner pipe
        
        
          d
        
        
          out, inner pipe
        
        
          Figure 2. Freeze pipe diameters to calculate hydraulic diameter.
        
        
          The hydraulic diameter for the annular space is:
        
        
          
            innerpip
          
        
        
          
            ,out
          
        
        
          
            outerpipe
          
        
        
          
            ,in
          
        
        
          
            hydraulic
          
        
        
          
            d
          
        
        
          
            d
          
        
        
          
            d
          
        
        
          
        
        
          
        
        
          (5)
        
        
          The Nusselt number Nu depends on the flow type – laminar
        
        
          or turbulent. To differ between the two flow types the Reynolds
        
        
          number Re can be used, which depends on the refrigerant flow
        
        
          velocity v
        
        
          F
        
        
          , the kinematic viscosity
        
        
          
        
        
          and the hydraulic diameter
        
        
          (VDI Heat Atlas 2010).
        
        
          
            F
          
        
        
          
            hydrauli
          
        
        
          
            dv
          
        
        
          
            Re
          
        
        
          
        
        
          
        
        
          
        
        
          (6)
        
        
          In the literature (Gnielinski 1995, VDI Heat Atlas 2010) it is
        
        
          generally mentioned that a full developed turbulent fluid flow in
        
        
          a pipe exists for Re > 10
        
        
          4
        
        
          . For Re < 2300 a laminar fluid flow
        
        
          occurs. In the range of 2300 < Re < 10
        
        
          4
        
        
          the transition from
        
        
          laminar to turbulent flow takes place. Furthermore, for all flow
        
        
          types a distinction has to be made between a modified fluid
        
        
          flow in the inlet area and a thermic and hydrodynamic fully
        
        
          developed fluid flow behind this area (VDI Heat Atlas 2010).
        
        
          Due to the spatial separation of the mechanical refrigeration
        
        
          plant and the inlet area of the freeze pipes, it can be assumed
        
        
          that the fluid flow reaching the inlet area is already fully
        
        
          developed.
        
        
          Moreover, the VDI Heat Atlas (2010) indicates the
        
        
          differentiation between flow inside a pipe and in a concentric
        
        
          annular gap. In this paper only the Nusselt numbers for the inner
        
        
          freeze pipe are outlined. The equations for the calculation in the
        
        
          annular gap can be found in VDI Heat Atlas (2010).
        
        
          In general the Nusselt number depends on the Reynolds
        
        
          number Re, the Prandtl number Pr, the inner pipe diameter d
        
        
          i
        
        
          and the length of the pipe l.Thus the Nusselt number in case of a
        
        
          laminar flow and a constant heat flux density along the freeze
        
        
          pipe can be calculated with:
        
        
          313
        
        
          31
        
        
          
            /
          
        
        
          
            /
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          3 3
        
        
          60
        
        
          9531 60 364 4
        
        
          
            i
          
        
        
          
            q,m
          
        
        
          
            ,
          
        
        
          
            l
          
        
        
          
            dPrRe
          
        
        
          
            ,
          
        
        
          
            ,
          
        
        
          
            ,
          
        
        
          
            Nu
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
            
        
        
          (7)
        
        
          In case of a turbulent flow, there is no need for a
        
        
          differentiation between the boundary conditions “constant wall
        
        
          temperature” and “constant heat flux density” since the Nusselt
        
        
          numbers are nearly equal. Thus the Nusselt number for
        
        
          turbulent flow is defined as:
        
        
           
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
        
        
           
        
        
          
        
        
          
        
        
          32
        
        
          1
        
        
          1 8 7121
        
        
          8
        
        
          
            i
          
        
        
          
            /
          
        
        
          
            m
          
        
        
          
            l
          
        
        
          
            d
          
        
        
          
            Pr / ,
          
        
        
          
            PrRe /
          
        
        
          
            Nu
          
        
        
          
        
        
          
        
        
          32
        
        
          
            /
          
        
        
          (8)
        
        
          with:
        
        
          
        
        
          
        
        
          2
        
        
          10
        
        
          51
        
        
          81
        
        
          
        
        
          
        
        
          
        
        
          
            , Re log ,
          
        
        
          (9)
        
        
          According to Gnielinski (1995) the following interpolation
        
        
          function for the transition region between laminar and fully
        
        
          turbulent flow should be used:
        
        
          
        
        
          
        
        
          4
        
        
          10
        
        
          2300
        
        
          1
        
        
          
            ,T,m
          
        
        
          
            ,L,m
          
        
        
          
            m
          
        
        
          
            Nu
          
        
        
          
            Nu
          
        
        
          
            Nu
          
        
        
          
        
        
          
        
        
          (10)
        
        
          with:
        
        
          1 0
        
        
          2300
        
        
          10
        
        
          2300
        
        
          4
        
        
          
        
        
          
        
        
          
        
        
          
        
        
          
            and
          
        
        
          
            Re
          
        
        
          Besides the Reynolds number the Prandtl number Pr is
        
        
          needed for the calculation of the Nusselt number. The Prandtl
        
        
          number characterizes the material properties of the refrigerant
        
        
          (kinematic viscosity
        
        
          
        
        
          , thermal conductivity
        
        
          
        
        
          F
        
        
          and volumetric
        
        
          heat capacity c
        
        
          F
        
        
          ) (Baehr and Stephan 2006):
        
        
          
            F
          
        
        
          
            F
          
        
        
          
            c Pr
          
        
        
          
        
        
          
        
        
          
        
        
          (11)
        
        
          2.2
        
        
          
            Numerical modeling
          
        
        
          For a realistic calculation of all heat transfer mechanisms
        
        
          described afore the use of numerical methods becomes
        
        
          necessary. To avoid a very fine discretization which causes long
        
        
          simulation times a seperate module “freezrefcap” for the
        
        
          calculation of the heat transfer processes within the freeze pipe
        
        
          has been developed in cooperation with Geophysica