JAXA Supercomputer System Annual Report April 2020-March 2021

Report Number: R20EA1601

Subject Category: Aeronautical Technology

PDF available here

• Responsible Representative: Toshiya Nakamura, Director, Aeronautical Technology Directorate, Structures and Advanced Composite Research Unit
• Contact Information: Yuichiro Aoki(aoki.yuichiro@jaxa.jp)
• Members: Yuichiro Aoki, Toshiyuki Kasahara, Hiroki Kawabe

Abstract

The aim of this study is to clarify the effect of manufacturing defects, such as gaps and overlaps, on the strength of CFRP laminates fabricated by automated fiber placement.

Reference URL

N/A

Reasons and benefits of using JAXA Supercomputer System

In order to properly evaluate manufacturing defects in CFRP laminates, precise finite element modeling is required. Also, geometric nonlinearity caused by local large deformation due to local stress concentration needs to be considered. Therefore, it takes long time to obtain analytical results. Parallel calculation of JAXA supercomputer system enables to reduce the total computation time.

Achievements of the Year

A two-dimensional mechanical model of the quasi-isotropic laminates with an arbitrary inclined gap is proposed and analytically solved using a super-position technique as the sum of a global uniform stress field with a virtual force at both ends of the gap and a local stress field caused by the virtual force. The local problem is approximately solved using a Green function technique. The stress field under a unidirectional load are obtained in a closed-form expression in which the effect of the tapered portions typically observed at both sides of the gap is incorporated. The present solution agreeing with the finite element solution shows that significant stress concentration occurs at the end portion of the gap.

Fig.1: Cross-sectional observation of a CFRP laminate with gaps

Fig.2: Overview of the analytical model of the gapped area

Fig.3: Comparison of stresses near the side edge: finite element method result (A) and present theoritical result (B)

Fig.4: Stress field along the side edge

Publications

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Usage of JSS

Computational Information

• Process Parallelization Methods: MPI
• Thread Parallelization Methods: Automatic Parallelization
• Number of Processes: 2 - 228
• Elapsed Time per Case: 10 Hour(s)

Resources Used(JSS2)

Fraction of Usage in Total Resources*1(%): 0.04

Details

Please refer to System Configuration of JSS2 for the system configuration and major specifications of JSS2.

*1: Fraction of Usage in Total Resources: Weighted average of three resource types (Computing, File System, and Archiver).

*2: Fraction of Usage：Percentage of usage relative to each resource used in one year.

Resources Used(JSS3)

Fraction of Usage in Total Resources*1(%): 0.03

Details

Please refer to System Configuration of JSS3 for the system configuration and major specifications of JSS3.

*1: Fraction of Usage in Total Resources: Weighted average of three resource types (Computing, File System, and Archiver).

*2: Fraction of Usage：Percentage of usage relative to each resource used in one year.

JAXA Supercomputer System Annual Report April 2020-March 2021