Mobility and Coalescence of Water Droplet Formed in Fuel Cells Overview Introduction Objectives Mathematical Modeling Sample Simulations Introduction A unit cell of PEMFC is composed of a membrane electrode assembly, two diffusion media, and bipolar plates. The diffusion medium needs to be optimized to enhance the cell performance. In cathode diffusion medium, the product water flows towards the channel through gasphase diffusion or liquidphase motion. Porous Cathode H2O H2 H+ Porous Anode O2 At high current densities, the liquid flow rate increases due to the increased condensation, and when the channel is at the local vapor saturation condition, liquid water flows out of diffusion medium and surface droplet are formed. Fiber Screens Stacked fiber screens, and the same exposed to water-vapor saturated atmosphere. Objective Characterization of the mobility of micro-drops in the diffusion medium. Growth of the micro drops through coalescence. Consider effect of: Initial droplet number density; Initial droplet size; Vapor diffusion rates; Rate of droplet onset; Growth rate of drops; Surface contact angles; Thickness of the membrane. Proposed Porous Model Mathematical Model Basic assumptions Governing equations Laminar flow ; incompressible and Newtonian fluid V 0 Continuity Momentum FV FVV P . F V Fb t f V .f 0 Free-surface tracking t Modified flow equations in presence of solid walls Finite volume method ; structured mesh ; Youngs algorithm ; volume fraction for walls Energy Equation- Enthalpy Method Original Energy Equation h 1 (V )h ( k T ) t Final Energy Equation h 1 1 (V )h ( h ) 2 t h 0: ks , 0 cs 0 h H f : 0, h Hf : 0 H k kl , f l cl cl h interphase cl Hf Tm solid cs T liquid Free Surface Tracking Step 1. Specify liquid domain using VOF method in a cell full of liquid f 1 in a cell with no liquid Define a function f f 0 0 f 1 for a cell partly filled with liquid Represent actual liquid domain by corresponding f values liquid Actual liquid region 0 0 .10 .38 .48 0 .25 .87 1 1 .12 .91 1 1 1 Volume of Fluid representation Modeling Solid Walls Step 1: Define a Volume Fraction 1 for a cell in the liquid 0 for a cell in the wall 0 1 for a cell partially occupied by the wall Step 2: Use instead of a stair-step model Step 3: Modify fluid flow equations Liquid 0.2 0.8 1 0 0.05 0.7 0 0 0.1 Wall Modified Fluid Equations Continuity, Momentum and VOF Equations V 0 F V F VV P . F V Fb t f (V .) f 0 t Sample Simulations Impaction of a water Drop on a fiber Droplet diameter: 2 mm 3.18 mm tube; 1 m/s offset 1.55 mm two perpendicular tubes (0.5 mm) no offset Code Validation Droplet : 2 mm, 1 m/s; Tube: 3.18 mm (0.125 in); Offset: 1.55 mm Code validation (continued) Droplet : 2 mm, 1 m/s; Tube: 3.18 mm (0.125 in); Offset: 1.55 mm Droplet impact with heat transfer Droplet flow through a modeled Porous Medium Radial Capillary A staggered array of perforated plates Draw back and coalescence:Drop Spacing 42 m ; Droplets coalesce Contact Angle 45o Contact Angle 120o Drop Spacing 44 m ; Contact Angle 120o Droplets do not coalesce Droplet Collisions Head- On Collisions Permanent Coalescence Reflexive Separation or Off-axis Collisions Permanent Coalescence Stretching Separation then Permanent Coalescence Stretching Separation Tearing or Droplet Coalescence Drop Collisions: Experiments vs. Simulations Experimental Numerical Coalescence collision of two drops. Off-Axis Collisions Tearing (Water, We=56, Re=2392, X=0.73 and =0.5) Thank you Summary Our 3D free surface code can simulate the detailes of the droplet dynamics in porous systems. Continuity and Momentum Two-step time discretization of momentum equation: ~ n n 1 n n 1 n V V n VV n F V G n Fb (i ) t F F n 1 ~ V V 1 n p n 1 (ii ) t F Step (i): evaluate convective, viscous and surface tension effects explicitly Step (ii): combine with continuity equation to obtain the Poisson pressure equation: ~ 1 V n 1 n p t F Free Surface Tracking Step 2. Use function f to advect the free surface to a new location at each time step ut f V .f 0 t u Step 3. Reconstruct the free surface shape at the new location using Youngs algorithm 0 n̂ .10 Obtain normal nˆ f / f .05 .20 .87 1 and use values of f : get free surface cutting planes Youngs’ 3D-VOF Interfaces - piecewise “planes” Interface plane is fitted within a single cell Interface slope and fluid position are determined from inspection of neighboring cells Pentagonal Section Youngs’ 3D - Cases Triangle Quadrilateral - A Pentagon Quadrilateral - B Hexagon Youngs’ VOF Implementation Surface Reconstruction Using f-field determined cell “normal” (i.e. n f ) f Determine “case” using normal Position plane with known slope based upon volume fraction Compute plane area and vertices Fluid Advection, Compute flux across cell side (case dependent) Operator Split (i.e. do for x, y and z sweeps) f V f 0 t General Solution Procedure 1. Specify initial surface geometry and velocities 2. Begin Cycle, increment time and repeat 2-6 until done n ~ 3. Explicitly update V V convective terms viscous terms surface tension terms 4. Implicitly calculateP n1 using ICCG Method 5. UpdateV n1 with P n1 and apply BCs 6. Advect f-field using Youngs VOF and re-apply BCs Nondimensional Parameters Impact Parameter ds V s Vr Weber Number X 2b sin We dl d s ds Vr b Relative Velocity Vr Vl 2 Vs2 2VlVs cos V dl X Vr Reflexive Separation (X=0) Fragmentat ion Stretching Separation (X>0) Size Ratio ds dl Head-on Collisions Separation (Water, We=58, Re=1127) 0 1 6 14 2 7 15 16 3 8 17 18 4 9 19 10 20 21 5 11 12 13 22 23 24 Off-axis Collisions Coalescence (Water, We=25, Re=740, X=0.7) 0 11 1 12 2 13 3 14 4 15 5 16 6 7 17 8 18 9 10 19 20