主催: 一般社団法人 日本機械学会
会議名: 2020年度 年次大会
開催日: 2020/09/13 - 2020/09/16
The crew safety at Launch Abort System (LAS) under the high impact load has been numerically investigated using the simplified Hybrid-III dummy model. We show that the simplified model has a good potential to reproduce the load reponse that matches with the experimental result by modifying the stress-strain curve that describes the deformation behavior in hip part.