Comparison of Strain Distribution Between Results of Flight Test and Finite Element Analysis
JAXA Supercomputer System Annual Report April 2018-March 2019
Report Number: R18EDA101S01
Subject Category: Aeronautical Technology
- Responsible Representative: Hitoshi Arizono, Aeronautical Technology Directorate, Structures and Advanced Composite Research Unit
- Contact Information: Hitoshi Arizono(arizono.hitoshi@jaxa.jp)
- Members: Hitoshi Arizono, Youichi Sano, Natsuki Tsushima
Abstract
Comparison of Strain Distribution Between Results of Flight Test and Finite Element Analysis
Reference URL
N/A
Reasons for using JSS2
Because complex real aircraft configuration is very expensive for simulation
Achievements of the Year
The strain distribution measured in the flight test was compared by loading the aerodynamic force of Hisho analyzed by JSS2 into the finite element model.
Publications
N/A
Usage of JSS2
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: N/A
- Number of Processes: 224
- Elapsed Time per Case: 10 Hour(s)
Resources Used
Fraction of Usage in Total Resources*1(%): 0.00
Details
Please refer to System Configuration of JSS2 for the system configuration and major specifications of JSS2.
| System Name | Amount of Core Time(core x hours) | Fraction of Usage*2(%) |
|---|---|---|
| SORA-MA | 32,977.08 | 0.00 |
| SORA-PP | 295.82 | 0.00 |
| SORA-LM | 80.01 | 0.04 |
| SORA-TPP | 0.00 | 0.00 |
| File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
|---|---|---|
| /home | 16.21 | 0.02 |
| /data | 162.12 | 0.00 |
| /ltmp | 3,320.31 | 0.28 |
| Archiver Name | Storage Used(TiB) | Fraction of Usage*2(%) |
|---|---|---|
| J-SPACE | 0.00 | 0.00 |
*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 2018-March 2019