We present a parallel numerical method of simulating the interaction of atoms with a strong laser field by solving the time-depending Schr?dinger equation(TDSE) in spherical coordinates. This method is realized by com...We present a parallel numerical method of simulating the interaction of atoms with a strong laser field by solving the time-depending Schr?dinger equation(TDSE) in spherical coordinates. This method is realized by combining constructing block diagonal matrices through using the real space product formula(RSPF) with splitting out diagonal sub-matrices for short iterative Lanczos(SIL) propagator. The numerical implementation of the solver guarantees efficient parallel computing for the simulation of real physical problems such as high harmonic generation(HHG) in these interaction systems.展开更多
为解决并行应用程序使用FFTW(Fastest Fourier Transform in the West)并行软件包所面临的计算规模难以扩展、数据结构变动大、实现不同数据结构间通信难度大、接口不确定等问题,在JASMIN框架内设计实现FFT并行解法器.该解法器封装了数...为解决并行应用程序使用FFTW(Fastest Fourier Transform in the West)并行软件包所面临的计算规模难以扩展、数据结构变动大、实现不同数据结构间通信难度大、接口不确定等问题,在JASMIN框架内设计实现FFT并行解法器.该解法器封装了数据分布存储、数据通信等并行计算细节,通过重新分布存储数据,调用一维FFT变换实现高维FFT的并行计算,并提供规范接口,支撑用户简便地实现FFT的并行计算.数值测试表明,该解法器具有很好的并行性能.该解法器已应用于激光等离子体成丝不稳定性的数值模拟并行程序,它在2048个处理器上的并行效率可达80%以上.展开更多
The use of Navier-Stokes simulation in the daily design process of multistage compressor requires extremely large computer resources. A less expensive alternate is the development of parallel numerical simulation on a...The use of Navier-Stokes simulation in the daily design process of multistage compressor requires extremely large computer resources. A less expensive alternate is the development of parallel numerical simulation on a workstations cluster for parallel distributed supercomputer. An average-passage model was introduced to include the unsteady flow effects and wake blockage and to make all of the flow variables are continues at the interface planes. A parallel Navier-Stokes solver has been developed for multistage high pressure ratio compressor based on domain decomposition methodology. This multiblade row solver was applied to analyze the flow field of the first 3 stage blade rows of a 7 stage high pressure ratio compressor at the design point.展开更多
基金Project supported by the National Natural Science Foundation of China(Grant Nos.11534004,11627807,11774131,and 11774130)the Scientific and Technological Project of Jilin Provincial Education Department in the Thirteenth Five-Year Plan,China(Grant No.JJKH20170538KJ)
文摘We present a parallel numerical method of simulating the interaction of atoms with a strong laser field by solving the time-depending Schr?dinger equation(TDSE) in spherical coordinates. This method is realized by combining constructing block diagonal matrices through using the real space product formula(RSPF) with splitting out diagonal sub-matrices for short iterative Lanczos(SIL) propagator. The numerical implementation of the solver guarantees efficient parallel computing for the simulation of real physical problems such as high harmonic generation(HHG) in these interaction systems.
文摘为解决并行应用程序使用FFTW(Fastest Fourier Transform in the West)并行软件包所面临的计算规模难以扩展、数据结构变动大、实现不同数据结构间通信难度大、接口不确定等问题,在JASMIN框架内设计实现FFT并行解法器.该解法器封装了数据分布存储、数据通信等并行计算细节,通过重新分布存储数据,调用一维FFT变换实现高维FFT的并行计算,并提供规范接口,支撑用户简便地实现FFT的并行计算.数值测试表明,该解法器具有很好的并行性能.该解法器已应用于激光等离子体成丝不稳定性的数值模拟并行程序,它在2048个处理器上的并行效率可达80%以上.
文摘The use of Navier-Stokes simulation in the daily design process of multistage compressor requires extremely large computer resources. A less expensive alternate is the development of parallel numerical simulation on a workstations cluster for parallel distributed supercomputer. An average-passage model was introduced to include the unsteady flow effects and wake blockage and to make all of the flow variables are continues at the interface planes. A parallel Navier-Stokes solver has been developed for multistage high pressure ratio compressor based on domain decomposition methodology. This multiblade row solver was applied to analyze the flow field of the first 3 stage blade rows of a 7 stage high pressure ratio compressor at the design point.
