Fluid analysis for CFD workshops
JAXA Supercomputer System Annual Report February 2025-January 2026
Report Number: R25EDA201G27
Subject Category: Aeronautical Technology
- Responsible Representative: Kazuyuki Nakakita, Aviation Technology Directorate, Fundamental Technology Research Unit
- Contact Information: Andrea Sansica(sansica.andrea@jaxa.jp)
- Members: David Lusher, Kenji Hayashi, Tomoaki Matsuzaki, Yoimi Kojima, Junpei Kakazu, Andrea Sansica
Abstract
Through our participation in various domestic and international workshops, we are advancing the predictive capabilities for full-aircraft configurations under stall conditions. Furthermore, we are establishing a set of best-practice guidelines aimed at maximizing both the robustness and accuracy of these numerical simulations.
Reference URL
N/A
Reasons and benefits of using JAXA Supercomputer System
For CFD workshops, it is necessary to use JAXA's supercomputers to perform a large number of calculations of three-dimensional complex shapes to achieve high accuracy.
Achievements of the Year
By conducting high-fidelity analyses focused on the CRM-HL configuration under stall conditions, we established numerical best-practices for simulating stall and buffet phenomena. Our research successfully identified specific sources of numerical error related to low-speed stall, particularly regarding the wake generated by slat brackets and flow separation on the flaps. Validation against Figure 1 demonstrates that FaSTAR consistently achieves the highest level of agreement with reference data and other state-of-the-art solvers. Furthermore, the JAXA experimental data utilized in this study will serve as the global reference for the international community at the 8th AIAA/NASA CFD Drag Prediction Workshop.
Fig.1: Comparison of lift coefficients and sectional pressure distributions across various solvers. FaSTAR results demonstrate high correlation with both numerical reference data and experimental results.
Publications
- Peer-reviewed papers
Markus Zauner, Andrea Sansica, Tomoaki Matsuzaki, Yoimi Kojima, Kosuke Uchida, and Atsushi Hashimoto, "In-Tunnel Delayed Detached-Eddy Simulations and Reynolds-Averaged Navier–Stokes Simulations of the NASA High-Lift Configuration of the Common Research Model", AIAA Journal 2025 63:9, 3700-3718
- Non peer-reviewed papers
[1] Andrea Sansica et al, "Assessment of High-Fidelity Numerical Simulations for the Characterization of CL-max Prediction on the High-Lift Configuration of the NASA CRM Including Wind-Tunnel Walls", NATO-AVT 391, Washington DC, May 2025
[2] Andrea Sansica, Brent W. Pomeroy, Bret Stanford, Daniella Raveh and Hadar Ben-Gida. "DPW-8/AePW-4 Buffet Working Group: An Overview of Mini Workshops 1 and 2," AIAA 2025-3159. AIAA AVIATION FORUM AND ASCEND 2025. July 2025.
- Oral Presentations
[1] Andrea Sansica et al, "Assessment of High-Fidelity Numerical Simulations for the Characterization of CL-max Prediction on the High-Lift Configuration of the NASA CRM Including Wind-Tunnel Walls", NATO-AVT 391, Washington DC, May 2025
[2] Andrea Sansica, Brent W. Pomeroy, Bret Stanford, Daniella Raveh and Hadar Ben-Gida. "DPW-8/AePW-4 Buffet Working Group: An Overview of Mini Workshops 1 and 2," AIAA 2025-3159. AIAA AVIATION FORUM AND ASCEND 2025. July 2025
[3] Andrea Sansica. "JAXA Contribution to DPW-8/AePW-4 Buffet Working Group for Test Case 2 using FaSTAR," AIAA SCITECH 2026. January 2026
[4] A. Sansica, D.J. Lusher, T. Matsuzaki. Contribution of JAXA to APC-10 using FaSTAR on the CRM high-lift configuration. 第57回流体力学講演会/第43回航空宇宙数値シミュレーション技術シンポジウム (July 2025)
- Other
APC-10 Workshop JAXA-SP-25-005, https://jaxa.repo.nii.ac.jp/records/2002405
Usage of JSS
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: N/A
- Number of Processes: 480 - 2304
- Elapsed Time per Case: 200 Hour(s)
JSS3 Resources Used
Fraction of Usage in Total Resources*1(%): 1.18
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 | 28936133.63 | 1.31 |
| TOKI-ST | 569455.26 | 0.59 |
| TOKI-GP | 0.00 | 0.00 |
| TOKI-XM | 1949.78 | 0.67 |
| TOKI-LM | 25825.21 | 1.95 |
| 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 | 1024.00 | 1.64 |
| /data and /data2 | 102400.00 | 0.67 |
| /ssd | 30720.00 | 1.87 |
| Archiver Name | Storage Used(TiB) | Fraction of Usage*2(%) |
|---|---|---|
| J-SPACE | 19.86 | 0.06 |
*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) | 2174.92 | 1.52 |
*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.
JAXA Supercomputer System Annual Report February 2025-January 2026
