The rebound behaviors of droplets impacting on a self-fabricated superhydrophobic brass surface (WCA=164.5°) were observed and studied by using high-speed-camera. In accordance with energy conversion, theoretical...The rebound behaviors of droplets impacting on a self-fabricated superhydrophobic brass surface (WCA=164.5°) were observed and studied by using high-speed-camera. In accordance with energy conversion, theoretical analysis of different behaviors and rebound mechanism were given. At lower velocities, three behaviors in different velocity ranges were observed: partial rebounding, entire rebounding and ejecting during rebounding. At higher velocities, such two behaviors as rebound after splashing and rebound, ejecting after splashing, occurred alternately and exhibited certain periodicity. A function to predict the critical impact velocity is derived from energy conservation condition, and the prediction values tally with the experimental values, with the maximum relative error about 14%.展开更多
Numerical research of flow past a circular cylinder with a splitter at the subcritical Reynolds number region of 5 × 10~4—9 × 10~4 was researched based on Computational Fluid Dynamics(CFD) through solving t...Numerical research of flow past a circular cylinder with a splitter at the subcritical Reynolds number region of 5 × 10~4—9 × 10~4 was researched based on Computational Fluid Dynamics(CFD) through solving twodimensional incompressible unsteady Reynolds-averaged Navier-Stokes(URANS) equations with the shear stress transport(SST) k-ω turbulence model. Three different grid resolutions were employed in the verification and validation study of the adopted turbulence model. Various fluid characteristics such as Strouhal number, lift coefficient of the cylinder and the splitter with respect to various splitter lengths and different Reynolds numbers were investigated. It was revealed that the lift coefficient ratio of the splitter over the cylinder remains near 1.6 when the splitter length is 1.5—4 times the cylinder's diameter. Vortex shedding is strongly inhibited when the splitter length is greater than a critical value of around four times the cylinder's diameter. The phase difference of the lift coefficient on the upper and lower surface of the splitter varies between-30?and 30?. The maximal lift coefficients are reached when the splitter length is about 2 times the cylinder's diameter. Besides, the splitter length has little influence on the separation angle around the cylinder.展开更多
基金supported by The National Natural Science Foundation of China (Grant No.51109178)Science and Technology Innovation Foundation of NWPU (Grant No.JC20120218)
文摘The rebound behaviors of droplets impacting on a self-fabricated superhydrophobic brass surface (WCA=164.5°) were observed and studied by using high-speed-camera. In accordance with energy conversion, theoretical analysis of different behaviors and rebound mechanism were given. At lower velocities, three behaviors in different velocity ranges were observed: partial rebounding, entire rebounding and ejecting during rebounding. At higher velocities, such two behaviors as rebound after splashing and rebound, ejecting after splashing, occurred alternately and exhibited certain periodicity. A function to predict the critical impact velocity is derived from energy conservation condition, and the prediction values tally with the experimental values, with the maximum relative error about 14%.
基金the National Natural Science Foundation of China(Nos.51179159 and 61572404)
文摘Numerical research of flow past a circular cylinder with a splitter at the subcritical Reynolds number region of 5 × 10~4—9 × 10~4 was researched based on Computational Fluid Dynamics(CFD) through solving twodimensional incompressible unsteady Reynolds-averaged Navier-Stokes(URANS) equations with the shear stress transport(SST) k-ω turbulence model. Three different grid resolutions were employed in the verification and validation study of the adopted turbulence model. Various fluid characteristics such as Strouhal number, lift coefficient of the cylinder and the splitter with respect to various splitter lengths and different Reynolds numbers were investigated. It was revealed that the lift coefficient ratio of the splitter over the cylinder remains near 1.6 when the splitter length is 1.5—4 times the cylinder's diameter. Vortex shedding is strongly inhibited when the splitter length is greater than a critical value of around four times the cylinder's diameter. The phase difference of the lift coefficient on the upper and lower surface of the splitter varies between-30?and 30?. The maximal lift coefficients are reached when the splitter length is about 2 times the cylinder's diameter. Besides, the splitter length has little influence on the separation angle around the cylinder.
