MASAMUNE-IMR consists of the Supercomputer (Cray XC50-LC and Cray CS-Storm 500GT) and Parallel computing and informatics server (HPE ProLiant DL360 Gen 10), etc. It is integrated by Hitachi, Ltd. The system configuration and specification are shown as below.
System Name | Supercomputer | Parallel Computing/ Informatics Server |
|
---|---|---|---|
Model | Cray XC50-LC | Cray CS-Storm 500GT | HPE ProLiant DL360 Gen10 |
Appearance | |||
total nodes | computing node:293nodes I/O node, etc : 27nodes |
29 nodes | 29 nodes |
CPU |
Intel Xeon Gold 6150
|
Intel Xeon Gold 6150
|
Intel Xeon Gold 6154
|
Accelerator | - |
NVIDIA Tesla V100 for PCIe
|
- |
memory size | 768 GiB/node | 768 GiB/node | 576 GiB/node |
Theoretical peak performance | 3.03 PFLOPS (CPU: 1.00 PFLOPS, GPU: 2.03 PFLOPS) |
100.22 TFLOPS | |
total number of CPU cores | 11,592 cores | 1,044 cores | |
total number of GPU cores | 1,484,800 cores (290 GPUs) | - | |
total memory size | 241.6 TiB | 16.3 TiB |
Nickname: MASAMUNE-IMR
MAterials science Supercomputing system for Advanced MUlti-scale simulations towards NExt-generation - Institute for Materials Research
Nickname “MASAMUNE-IMR” is given to the supercomputing system of CCMS. This nickname is from “Masamune Date” who was the first lord of Sendai in the 17th century and dispatched the sailing ship “San Juan Bautista” in 1613 towards the world from Sendai. “Masamune Date” is drew on the front panel of our supercomputer by Sumi-E Artist OKAZU, with the letters “MASAMUNE-IMR” . This “Masamune Date” on the front panel is looking ahead to the next-generation materials science of the world from Sendai. In the nickname, “MASAMUNE-IMR” , we express our hope that creative and innovative achievements of the advanced multi-scale simulations on materials science obtained by our supercomputing system will give great impacts towards the next-generation from Sendai to the world.
※ “MASAMUNE-IMR” is a registered trademark of Tohoku University.
In recent years, precision micromechanical systems used in drones, robots, automobiles, medical instruments, etc., have been developing at an accelerating rate, in response to the growing demands for them. However, when micromechanical systems are driven in a drone, robot, automobile, medical instrument, etc., the materials of the micromechanical systems rub against each other causing wear, which seriously damages their accuracy and durability. Especially, because micromechanical systems are extremely small in size, even a very small amount of wear, which is not a problem in normal size mechanical systems such as engines, motors, transmissions, etc., causes great damages to the entire systems. Therefore, it is strongly required to reduce the amount of wear to the utmost limit.
To prolong the life of mechanical systems and to improve their durability by solving the above problem, it is necessary to establish a theoretical law that can quantitatively predict how much wear will occur depending on the materials and usage conditions before conducting experimental research. However, in micromechanical systems, this wear phenomena occur at friction interfaces of tens of nanometers. Therefore, unlike visible wear which occurs in normal size mechanical systems such as engines, motors, and transmissions, nano-scale wear which cannot be seen by the naked eyes and is dominated by atomistic chemical reactions is the main factor in the micromechanical systems. Therefore, it has long been pointed out that the conventional wear prediction law for normal size mechanical systems cannot be applied to micromechanical systems, however this problem has not been solved for a long time.
Therefore, by developing a reactive molecular dynamics simulator that can elucidate complicated multi-physics phenomena including chemical reactions on the supercomputer “MASAMUNE-IMR”, chemical reaction mechanisms which induce wear at the friction interface of micromechanical systems are clarified. By applying the reaction rate theory to the above chemical reaction mechanisms, we proposed a non-empirical atom-by-atom wear law for predicting the wear amounts of materials for micromechanical systems. Furthermore, we simulated the wear amount of diamond-like carbon by reactive molecular dynamics method using the supercomputer and then proved that the very simple wear amount prediction law constructed in this study is able to quantitatively predict the wear amount obtained by long-time molecular dynamics calculations using the supercomputer. This result contributes not only to prolonging the life of micromechanical systems but also to the prevention of breakdowns and accidents.
Fig. Wear amounts of diamond-like carbon obtained by wear law and atomistic molecular dynamics simulation.
- Wear amounts of (a) rough-surfaces and (b) ball-on-disk contacts show different dependence of loads. These figures prove that the very simple wear amount prediction law constructed in this study is able to quantitatively predict the wear amount obtained by long-time molecular dynamics calculations using the supercomputer.
Yang Wang, Jingxiang Xu, Yusuke Ootani, Nobuki Ozawa, Koshi Adachi, and Momoji Kubo
Adv. Sci., 8 (2021) Art.No.2002827, https://doi.org/10.1002/advs.202002827
In a magnetic material, magnetic moments align themselves with their neighbors in very specific formations. While the magnetic structure determines the physical properties of magnets, accurate prediction of the spin configuration is one of the grand challenges in solid state physics. This is due to the presence of many degrees of freedom in the system. In this study, we device the cluster multipole (CMP) theory to treat the degrees of freedom in a physically meaningful way, and create an exhaustive list of candidate magnetic structures for which we performed a high-throughput calculation with ~3,000 possible magnetic structures. With the combination of the CMP theory and the local spin-density approximation (LSDA) for noncollinear magnetism, our study lays a solid foundation for the ab initio predictions of various magnetic properties by showing that (1) the CMP expansion administers an exhaustive list of candidate magnetic structures, (2) CMP + LSDA can narrow down the possible magnetic configurations to a handful of computed configurations, and (3) LSDA reproduces the experimental magnetic configurations with an accuracy of ~0.5μB.
M.-T. Huebsch, T. Nomoto, M.-T. Suzuki, and R. Arita
Phys. Rev. X, 11 (2021) Art.No.011031, DOI:https://doi.org/10.1103/PhysRevX.11.011031
The upper panel shows the 2D map of the local free energy of Ni-Ti alloys where at most two interstitial atoms are considered in the tetrahedron approximation. The values for the compositions NinTim with n + m ≤ 6 are determined by first-principles calculations. The Ni concentration, φNi, and the Ti concentration, φTi, are discretized as n ≤ φNi < n + 1 and m ≤ φTi < 𝑚 + 1, and each square box corresponds to one ( n, m ).
The lower panel shows he steady spatial distributions of the Ni concentration, φNi, calculated by the first-principles phase field method only using the local free energy shown in the upper panel without any empirical parameter for Ti-45at%Ni, Ti-48at%Ni, Ti-50at%Ni, Ti-52at%Ni, and Ti-55at%Ni. The resulting patterns are almost the same as those without considering interstitial atoms, though some of the cuboidal or angular precipitations are rotated, and orange crosses appear around the yellow spots for Ti-50at%Ni. This rotation is reasonable, because no rotation along with the simulation cell axes is an artifact when we did not consider the interstitial atoms. The interstitial configurations do not appear in the final microstructure although they could influence the dynamics.
Kaoru Ohno, Monami Tsuchiya, Riichi Kuwahara, Ryoji Sahara, Swastibrata Bhattacharyya, and Thi Nu Pham
Comp. Mat. Sci., 191 (2021) Art.No.110284, DOI:https://doi.org/10.1016/j.commatsci.2021.110284
By ab initio simulations, the degree of lattice distortion for Mo-added NiCoCrFe-based high-entropy alloys (HEAs) was precisely evaluated. The atomic volumes and bond lengths (BL) of the constituent elements in the off-equiatomic Mox HEAs (x = 0, 0.1, 0.2, 0.3, 0.4, 0.475, and 0.54) ascended with increasing the Mo content. However, the increase in the mean BL(BL)was not significant (0.2% per at%Mo), indicating that the effect of lattice expansion on the solid-solution strengthening was minimal. In contrast, the misfit parameter σBL, which corresponds to the standard deviation of BL, increased significantly at first, changed slowly after the Mo0.3 HEA, and peaked at the Mo0.475 (Ni1.8Co0.95Cr0.8Fe0.25Mo0.475) HEA. This indicates that Mo atoms induce large lattice distortion locally in the NiCoCrFe-based solid-solution HEAs. The most severe lattice distortion in the Mo0.475 HEA resulted in the highest energy barrier for the dislocation glide. The experiment validated the highest yield stress in the homogenized Mo0.475 HEA.
J. Li, K. Yamanaka, and A. Chiba
Mater. Sci. Eng. A, 817 (2021) Art.No.141359, DOI:https://doi.org/10.1016/j.msea.2021.141359