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Materials Science in Additive Manufacturing                 In situ electromagnetic field manipulation during LMD


              The high-energy beam formed by semiconductor lasers   2.3.4. Buoyancy equation for heat
            is unevenly distributed, exhibiting a trend of high energy   Thermal buoyancy is typically generated by density
            density in the center that gradually decreases toward the   variations caused by temperature changes in liquid metals.
            periphery. The Gaussian distribution laser heat source   The  density  gradient  is  related  to  the  expansion  of  the
            model is adopted and expressed as follows: 25      liquid metal, commonly represented by Boussinesq. It

                                                               is assumed that the density of the fluid is constant in
                               (    2   2  
                                  −
                    P
                  ωη        ω 2     xv t) +  y           the time derivative and convective terms, with only the
                                    s
            Q laser  =  2  r π  l  exp  −  r  2      (IX)    buoyancy  term  affected  by density fluctuations.  The
                          
                     l
                                            
                                   b                         relevant equations are simplified, and the spatial variation
                                                               of density is confined to the buoyancy term. The equation
                                                               for buoyancy is as follows: 32
              Where P represents the laser power, ω  is the Gaussian
                                             2
            distribution coefficient of the laser, ɳ is the laser utilization   F buoyancy  = ρ gβ(T-T)  (XIV)
                                                                              l
                                                                       l
                                         l
            efficiency, and r  is the effective laser radius.    Where  ρ represents the  density of  the metal at  the
                        b
                                                                         l
              Convective heat transfer exists in the four lateral surfaces   liquidus temperature T, and β is the thermal expansion
                                                                                  l
            of the substrate, while both convective and radiative heat   coefficient of the metal.
            transfer occurs on the substrate surface. Heat dissipation
            through convection and radiation is represented by the   2.3.5. Electromagnetic force equation
            following equation: 28                             The movement of conductive particles in an electromagnetic
                                                               field produces current density during the scanning process
                            h TT− ) +⋅ (
                                                 4
                                              4
                                                T
            Q losses  = Q con  + Q rad  =⋅(  0  εσ b ⋅  T − )  (X)  of the laser head. The electromagnetic force is generated
                                                 0
                                                               under the influence of an externally applied longitudinal
                                                               electromagnetic field, and the electromagnetic force in the
              Where  h represents  the convective  heat  transfer
            coefficient, T is the real-time wall surface temperature, T    molten pool can be expressed by the following equation:
                                                          0
            is the ambient temperature, ε is the surface emissivity of   F = J×B                         (XV)
            the material, and σ is the Stefan-Boltzmann constant.  Where F represents the Lorentz force, J is the current
            2.3.3. Surface force equation                      density vector, and B is the magnetic flux density vector.
            The numerical model includes two surface tensions: (i) the   2.4. Material thermophysical parameters
            surface tension f  generated due to the curvature between   The thermophysical parameters of the Ti-6Al-4V
                         S,n
            argon gas and the liquid molten pool interface, which acts   alloy used in the simulation are listed in  Table  1. The
            perpendicular to the surface, and (ii) the Marangoni shear   parameters are determined by commercial material
            stress f  arises from the uneven thermal distribution on
                 S,t
            the molten pool surface, resulting in larger temperature   Table 1. Physical parameters used in the simulation
            gradients tangent to the free surface. The specific equation
            for surface forces is presented as follows: 29     Property                     Value      Unit
            F  = f  + f  = σ.κ.n+∇  σ                  (XI)    Density (ρ)                   4440      kg∙m -3
                              t
                    S,t
             S
                S,n
                                                                                                         -1
                                                                                             -3
              Where  σ represents surface tension,  κ is surface   Dynamic viscosity (μ )  2.6×10  (1878 K)  kg∙m ∙s -1
                                                                             0
            curvature, and n is a vector perpendicular to the surface.   Solidus temperature (TS)  1878  K
            The  equations  for  surface  tension  and  Marangoni  shear   Liquidus temperature (TL)  1928  K
            stress are as follows: 30,31                       Specific heat capacity (cp)  550 (297 K)  J∙kg ∙K -1
                                                                                                         -1
                                                                                                         -1
                                                               Thermal conductivity (k)   5.74 (297 K)  W∙m ∙K -1
                ∇γ
            n =                                       (XII)    Latent heat of fusion (L)    2.92×10 5  J∙kg -1
                ∇γ                                             Thermal expansion coefficient (β)  1.6×10 -4  K -1
                                                               Surface tension (σ)        1.65 (1928 K)  N∙m -1
                  dσ      dσ
                                        T
            ∇ σ =  dT  ∇ T  =  dT   Tn  ⋅∇ )       (XIII)   Surface tension coefficient     dσ    −2.44×10 -4  N∙m ∙K -1
                             ∇− ⋅(n
                                                                                                         -1
                             
                      t
              t
                     dσ                                                             dT 
              Where       represents  the temperature  coefficient of                            -8
                     dT                                        Stefan-Boltzmann constant (σS)  5.67×10   K
            surface tension.                                   Radiation emissivity (ε)      0.8         -
            Volume 4 Issue 1 (2025)                         5                              doi: 10.36922/msam.8332
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