Computational Performance of Progressive Damage Analysis of Composite Laminates using Abaqus/Explicit with 16 to 512 CPU Cores

Bergan, A C

关键词: COMPOSITE STRUCTURES;    COMPUTER PROGRAMS;    COST ANALYSIS;    DAMAGE ASSESSMENT;    FINITE ELEMENT METHOD;    LAMINATES;    PREDICTION ANALYSIS TECHNIQUES;    STRUCTURAL DESIGN;    DEGREES OF FREEDOM;   

RP-ID  :  NASA/TM-2019-220251,L-20998,NF1676L-32380

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The computational scaling performance of progressive damage analysis using Abaqus/ Explicit is evaluated and quantified using from 16 to 512 CPU cores. Several analyses were conducted on varying numbers of cores to determine the scalability of the code on five NASA high performance computing systems. Two finite element models representative of typical models used for progressive damage analysis of composite laminates were used. The results indicate a 10 to 15 times speed up scaling from 24 to 512 cores. The run times were modestly reduced with newer generations of CPU hardware. If the number of degrees of freedom is held constant with respect to the number of cores, the model size can be increased by a factor of 20, scaling from 16 to 512 cores, with the same run time. An empirical expression was derived relating run time, the number of cores, and the number of degrees of freedom. Analysis cost was examined in terms of software tokens and hardware utilization. Using additional cores reduces token usage since the computational performance increases more rapidly than the token requirement with increasing number of cores. The in- crease in hardware cost with increasing cores was found to be modest. Overall the results show relatively good scalability of the Abaqus/Explicit code on up to 512 cores.