Supplementary materials to Pinhole formation from liquid metal microdroplets impact on solid surfaces Hao Yi, Le-hua Qi a), Jun Luo, Yuanyuan Jiang, and Weiwei Deng b) The heat transfer analysis performed here applies classic model and theory that can be found in many heat transfer textbooks such as Fundamentals of Heat and Mass Transfer, 7th edition by Incropera and Dewitt, Wiley, 2011, which is referred as (Incropera and Dewitt, 2011) hereafter. Convection heat transfer coefficient h For free falling liquid droplets, the scaling law for Nusselt (Nu) number is (Incropera and Dewitt, 2011, p465): Nu=2+0.6Re0.5Pr1/3, where Re is the Reynolds number and Pr is the Prandtl number. Typical experimental parameters (droplet diameter 500 µm, droplet velocity 1m/s, Pr=0.67) in this work correspond to Re=18 and Nu=4.2. The definition of Nusselt number is: Nu=hD/kg, where D is the droplet diameter, kg is the thermal conductivity of the gas. For Argon, kg =0.016 W/(mK), and we obtain h=135 W/(m2K). Isothermal approximation Next we evaluate the Biot number, which is the ratio of conduction heat transfer resistance within the droplet to the convective heat transfer resistance: Bi=hD/kd, where kd is the thermal conductivity of the droplet (kd =200 W/(mK)). Thus Bi is estimated to be about 310-4<<1, which suggests the droplet is isothermal, i.e. the temperature is uniform within the droplet. Transient heat transfer time constant For an isothermal object, one can use the lumped capacitance model to describe the temperature history. The transient cooling time constant tc can be estimated using: tc=mcd/hA, where m is the mass of the droplet, cd is the specific heat capacity of molten droplet, A is the surface area of the droplet. Typical experimental parameters in this work (cd=1086 J/kg/K, h=135 W/m2/K) yield tc =1.4 s, which is much longer than the droplet travel time (0.1 s) prior to impact. a) qilehua@nwpu.edu.cn, b) weiwei@vt.edu Heat conduction through the gas layer The typical geometry of the gas layer under the impacting droplet is ~100 µm in diameter and ~2 µm thick. Assume the temperatures of the two sides of the gas layer is Td=1023K (droplet) and Ts=303K (substrate), one can estimate the conduction heat transfer rate from the droplet to the substrate is ~0.05W. The latent heat of the droplet is 0.6 J based on specific latent heat of aluminum (400kJ/kg) and the droplet mass (1.510-7kg). This suggests that it will take at least ~ 100 ms to fully solidify the droplet if the gas layer is preserved. Instantaneous contact temperature To estimate the temperature of the aluminum/brass interface (Ti) immediately upon contact, we apply the model of two infinitely large objects of different temperatures that are suddenly in contact (Incropera and Dewitt, 2011, p315): (kc)1d/ 2 Td (kc)1s/ 2 Ts , Ti (kc)1d/ 2 (kc)1s/ 2 where k, , and c are the thermal conductivity, density, and specific heat respectively (subscript d refers to the droplet; subscript s refers to the substrate). For typical experimental conditions: kd = 200 W/(mK), d=2300 kg/m3, cd=1086 J/kg/K, ks = 109W/(mK), s=8500 kg/m3, cs=380 J/kg/K, Td=1023K, and Ts=303K: Ti=694K, which is below the melting point of Aluminum (933K). This implies that the thin layer of metal near the interface will be solidified immediately upon direct contact without gas cushion layer. Note that although the droplet may not be considered infinitely large, the interfacial temperature can only be overestimated and will not change the conclusion that Ti is below the melting point of aluminum.