Numerical analysis on combustion instability considering spray response
JAXA Supercomputer System Annual Report February 2024-January 2025
Report Number: R24EDA201C30
Subject Category: Aeronautical Technology
- Responsible Representative: Junichi Kazawa, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub
- Contact Information: Kazuaki Matsuura, Japan Aerospace Exploration Agency, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub.
- Members: Kazuaki Matsuura, Yuta Sasaki, Kodai Kato, Yoshio Zama
Abstract
Numerical analysis on combustion instability considering spray response is performed to clarify phenomena and improve prediction capability of CFD in combustion instabilities.
Reference URL
N/A
Reasons and benefits of using JAXA Supercomputer System
Phenomena on spray combustion require a high calculation load, and the use of super computer is necessary.
Achievements of the Year
Numerical simulations were performed to investigate combustion instabilities on a coaxially-staged lean-burn fuel injector.
For response of fuel flow rate to back pressure oscillation, a quasi-steady-type response model was employed.
Effects of pilot fuel splits (ratio of pilot fuel flow rate to overall) on frequencies and amplitudes of pressure oscillations in the combustor were investigated.
An example of such results is shown in Figure 2.

Fig.2: Effects of pilot fuel splits on frequencies and amplitudes of pressure oscillations in combustion instabilities.
Publications
N/A
Usage of JSS
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: N/A
- Number of Processes: 512
- Elapsed Time per Case: 160 Hour(s)
JSS3 Resources Used
Fraction of Usage in Total Resources*1(%): 0.30
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 | 7895988.96 | 0.36 |
TOKI-ST | 5437.25 | 0.01 |
TOKI-GP | 0.00 | 0.00 |
TOKI-XM | 0.00 | 0.00 |
TOKI-LM | 5.73 | 0.00 |
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 | 124.50 | 0.08 |
/data and /data2 | 115158.33 | 0.55 |
/ssd | 30720.00 | 1.65 |
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.
ISV Software Licenses Used
ISV Software Licenses Used(Hours) | Fraction of Usage*2(%) | |
---|---|---|
ISV Software Licenses(Total) | 49.60 | 0.03 |
*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.
JAXA Supercomputer System Annual Report February 2024-January 2025