Integrated Simulation over aircraft, rotorcraft and engines
JAXA Supercomputer System Annual Report February 2024-January 2025
Report Number: R24EDA201G21
Subject Category: Aeronautical Technology
- Responsible Representative: Atsushi Hashimoto, Aviation Technology Directorate, Aviation Technology Directrate, XANADU Project Team
- Contact Information: Taisuke Nambu, Aviation Technology Directorate, Fundamental Aeronautics Research Unit(nambu.taisuke@jaxa.jp)
- Members: Hirokazu Higashida, Manabu Hisida, Atsushi Hashimoto, Mami Hayakawa, Kenji Hayashi, Tomoaki Ikeda, Takashi Ishida, Masatoshi Kanayama, Ryohei Kirihara, Masashi Kanamori, Takuhito Kuwabara, Shingo Matsuyama, Taisuke Nambu, Hideji Saiki, Kei Shimura, Kanako Yasue, Hiroki Yao, Andrea Sansica
Abstract
In this study, with the aim of shortening the development period and reducing costs in aircraft development, we are conducting research and development on advanced Model-Based Development (MBD: Model-Based Development) and Model-Based Systems Engineering (MBSE) collaboration technologies with MBD Due to the reorganization of research cards, this fiscal year, we are conducting research and development focused on engine analysis technology under this project code.
As part of the research and development of engine analysis technology, we are conducting research on the advancement of the Cartesian grid CFD solver HINOCA-AE and the Many-block method, which is a unstructured grid method.
Reference URL
N/A
Reasons and benefits of using JAXA Supercomputer System
JSS is necessary to complete large scale numerical simulations of unsteady phenomena and to understand it in short time span.
Achievements of the Year
The main achievements of this fiscal year are the improvement of accuracy through the advancement of the combustion model implemented in HINOCA-AE and the enhancement of usability. The combustion model was refined based on the Flamelet method, and its accuracy was validated across multiple combustors. In several cases, it was confirmed that the exhaust temperature error could be kept within 100 K. Additionally, it was verified that grid generation from drawing data could be completed within a few days (or within a few hours for minor shape modifications), and the procedure was documented in a manual.
Publications
- Oral Presentations
Taisuke Nambu, Hiroki Yao, Takuhito Kuwabara, Ryohei Kirihara and Yasuhiro Mizobuchi, Research and Development of a Combustion Flow Analysis Program for Reciprocating Engines Using the Cartesian Grid and an Immersed Boundary Method,19th International Conference of Numerical Combustion
Usage of JSS
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: OpenMP
- Number of Processes: 1 - 8192
- Elapsed Time per Case: 480 Hour(s)
JSS3 Resources Used
Fraction of Usage in Total Resources*1(%): 1.22
Details
Please refer to System Configuration of JSS3 for the system configuration and major specifications of JSS3.
System Name | CPU Resources Used(Core x Hours) | Fraction of Usage*2(%) |
---|---|---|
TOKI-SORA | 32811678.21 | 1.50 |
TOKI-ST | 1616.10 | 0.00 |
TOKI-GP | 0.00 | 0.00 |
TOKI-XM | 0.00 | 0.00 |
TOKI-LM | 533.88 | 0.04 |
TOKI-TST | 0.00 | 0.00 |
TOKI-TGP | 0.00 | 0.00 |
TOKI-TLM | 0.00 | 0.00 |
File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
---|---|---|
/home | 1487.12 | 1.00 |
/data and /data2 | 152594.99 | 0.73 |
/ssd | 33648.33 | 1.80 |
Archiver Name | Storage Used(TiB) | Fraction of Usage*2(%) |
---|---|---|
J-SPACE | 13.86 | 0.05 |
*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.
ISV Software Licenses Used
ISV Software Licenses Used(Hours) | Fraction of Usage*2(%) | |
---|---|---|
ISV Software Licenses(Total) | 3.45 | 0.00 |
*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.
JAXA Supercomputer System Annual Report February 2024-January 2025