Improvement of numerical analysis for internal flow with complicated configuration inside aero-engine
JAXA Supercomputer System Annual Report April 2018-March 2019
Report Number: R18EA2120
Subject Category: Aeronautical Technology
- Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit
- Contact Information: Shigeru Kuchiishi(kuchi-ishi.shigeru@jaxa.jp)
- Members: Shunji Enomoto, Junichi Kazawa, Atsushi Hashimoto, Takashi Ishida, Shigeru Kuchiishi, Mitsumasa Makida, Hiroki Ugajin, Taisuke Nambu, Manabu Hisida, Rika Yamada, Keiji Ueshima, Yuuhi Tanaka, Naoki Tani
Abstract
Unstructured-grid flow solver FaSTAR-Move and grid generator BOXFUN are applied to aero-engine elements with complicated configuration (such as linear and rotating cascades). Through the calculation, these programs are tested and investigated for the deficiency and future issue for improvement of accuracy.
Reference URL
N/A
Reasons for using JSS2
Aiming to do large scale calculation in the future, programs should be tested under the same computational environment.
Achievements of the Year
Steady Reynolds averaged Navier-Stokes (RANS) calculations were performed for the transonic compressor, Rotor 67 and the cooled turbine cascade, T106A using FaSTAR-Move. The converged solutions has been obtained and validated.
Publications
N/A
Usage of JSS2
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: N/A
- Number of Processes: 16 – 512
- Elapsed Time per Case: 12 Hour(s)
Resources Used
Fraction of Usage in Total Resources*1(%): 0.11
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 | 859,332.27 | 0.11 |
SORA-PP | 3,785.42 | 0.03 |
SORA-LM | 0.00 | 0.00 |
SORA-TPP | 0.00 | 0.00 |
File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
---|---|---|
/home | 162.23 | 0.17 |
/data | 22,808.39 | 0.40 |
/ltmp | 4,858.74 | 0.42 |
Archiver Name | Storage Used(TiB) | Fraction of Usage*2(%) |
---|---|---|
J-SPACE | 9.64 | 0.34 |
*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