物理学报2017，Vol.66Issue(11)：188-196,9.DOI:10.7498/aps.66.114701
一种滑移区气体流动的格子Boltzmann曲边界处理新格式
A new curved boundary treatment in lattice Boltzmann method for micro gas flow in the slip regime
摘要
Abstract
A new curved boundary treatment in lattice Boltzmann method is developed for micro gas flow in the slip regime.The proposed treatment is a combination of the nonequilibrium extrapolation scheme for curved boundary with noslip velocity condition and the counter-extrapolation method for the velocity and its normal gradient on the curved boundary.Taking into consideration the effect of the offset between the physical boundary and the closest grid line,the new treatment is proved to be more accurate than the traditional half-way diffusive bounce-back (DBB) scheme.The present treatment is also more applicable than the modified DBB scheme because the specific gas-wall interaction parameters need to be determined to ensure the validation of the modified DBB scheme.The proposed boundary treatment is implemented to simulate the benchmark problems,which include a Poiseuille flow in the aligned/inclined micro-channel,a flow past a inicrocylinder and a microcylindrical Couette flow.The results and conclusions are summarized as follows.l) The force-driven Poiseuille flow in an aligned microchannel is simulated separately with different values of wallgrid offset qδx (q =0.25,0.5,0.75,1.0).With the consideration of the wall-grid offset,the numerical results with the new boundary treatment show good agreement with the analytical solut7ons.However,the results obtained by using the half-way DBB scheme only accord well with the analytical solutions under the condition of a fixed wall-grid offset (q =0.5).2) To demonstrate the capability of the present treatment in dealing with gas flow in a more complex geometry,the force-driven Poiseuille flow in a micro-channel is investigated separately with different inclined angles.The present numerical results fit well with the analytical solutions.However,the discrepancy between the results obtained with the half-way DBB scheme and the analytical solutions can be clearly observed near the inclined boundaries.3) The gas flow past a microcylinder is simulated to prove that the present treatment can deal with the curved boundary.The slip velocity profile along the micro cylinder periphery obtained with the present treatment accords well with the available data in the published literature.However,the results obtained with the half-way DBB scheme show lower values than the results from the published work.4) In the simulations of the microcylindrical Couette flow between two coaxial rotating cylinders for different Knudsen numbers the results obtained by using the present treatment show excellent agreement with the analytical solutions.However,the results obtained with the half-way DBB scheme and the modified DBB scheme deviate obviously from the analytical solutions near the inner and outer cylindrical walls,respectively.In summary,the new boundary treatment proposed in this work is capable of dealing with the complex gas-solid boundary in the slip regime.The new treatment has a higher accuracy than the half-way DBB scheme and shows a better applicability than the modified DBB scheme.关键词
曲边界/格子Boltzmann方法/滑移区/微气体流动Key words
curved boundary/lattice Boltzmann method/slip regime/micro gas flow引用本文复制引用
顾娟,黄荣宗,刘振宇,吴慧英..一种滑移区气体流动的格子Boltzmann曲边界处理新格式[J].物理学报,2017,66(11):188-196,9.基金项目
Project supported by the National Natural Science Foundation of China (Grant Nos.51536005,51521004).国家自然科学基金(批准号:51536005,51521004)资助的课题. （Grant Nos.51536005,51521004）
