TY  - RPRT
TI  - Computational Performance of Progressive Damage Analysis of Composite Laminates using Abaqus/Explicit with 16 to 512 CPU Cores
AU  - Bergan, A. C.
PY  - 2019
UR  - https://ntrs.nasa.gov/citations/20190001427
ID  - 20190001427
ER  -