Simulation of High-Speed Rotorcraft
JAXA Supercomputer System Annual Report February 2025-January 2026
Report Number: R25EDA201C20
Subject Category: Aeronautical Technology
- Responsible Representative: Kanako Yasue, Aviation Technology Directorate, Aviation Integration Innocation Hub
- Contact Information: Hideaki Sugawara(sugawara.hideaki@jaxa.jp)
- Members: Fumihiro Kajiwara, Yuki Kishi, Keita Kimura, Hideaki Sugawara, Ryo Takahashi, Yasutada Tanabe, Kanako Yasue
Abstract
This study investigates technologies for high-speed rotorcraft. The objectives are to enhance main rotor performance and reduce airframe drag to enable high-speed flight. To improve rotor performance, CFD-based optimization and advanced insights into rotor aerodynamics are employed. For airframe drag reduction, non-streamlined components, such as the rotor hub, are examined, with the aim of developing effective drag-reduction devices.
Reference URL
N/A
Reasons and benefits of using JAXA Supercomputer System
To perform a large number of computational simulations, an efficient high-performance computer is required.
Achievements of the Year
Previously developed hub drag reduction technologies were extended to a medium-sized helicopter model to assess their effectiveness at the system level beyond component-level evaluations. A full-configuration CFD analysis was conducted to decompose the drag components, quantify the contribution of hub drag to the total drag, and identify the primary drag sources. Based on these analyses, drag reduction devices were developed, and their effectiveness was demonstrated through both CFD simulations and wind tunnel experiments.
Publications
N/A
Usage of JSS
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: OpenMP
- Number of Processes: 480 - 1440
- Elapsed Time per Case: 336 Hour(s)
JSS3 Resources Used
Fraction of Usage in Total Resources*1(%): 0.82
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 | 12967840.28 | 0.59 |
| TOKI-ST | 2439624.39 | 2.53 |
| TOKI-GP | 0.00 | 0.00 |
| TOKI-XM | 0.00 | 0.00 |
| TOKI-LM | 19.82 | 0.00 |
| TOKI-TST | 495122.61 | 8.09 |
| TOKI-TGP | 0.00 | 0.00 |
| TOKI-TLM | 0.00 | 0.00 |
| File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
|---|---|---|
| /home | 0.00 | 0.00 |
| /data and /data2 | 102400.00 | 0.67 |
| /ssd | 0.00 | 0.00 |
| Archiver Name | Storage Used(TiB) | Fraction of Usage*2(%) |
|---|---|---|
| J-SPACE | 6.42 | 0.02 |
*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) | 563.37 | 0.39 |
*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.
JAXA Supercomputer System Annual Report February 2025-January 2026
