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Acoustic Liner Program for future High-bypass-ratio Aircraft engines(Development of combustor)

JAXA Supercomputer System Annual Report February 2024-January 2025

Report Number: R24EDA101C39

Subject Category: Aeronautical Technology

PDF available here

  • Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate,Aviation Environmental Sustainability Innovation
  • Contact Information: Naoyuki Okamura(okamura.naoyuki@jaxa.jp)
  • Members: Taisuke Nambu, Hideji Saiki

Abstract

In this project, we will apply next-generation acoustic liner to combustor. To perform the numerical analysis of combustor with the acoustic liner by using HINOCA-AE which is CFD solver for aircraft engine combustors.

Reference URL

N/A

Reasons and benefits of using JAXA Supercomputer System

We have designed the combustor by using hydrogen fuel. To differ from the flow field of jet fuel, we need to investigate the flow field of hydrogen fuel on the design phase.

Achievements of the Year

Our numerical analysis is focused on the flow field of the inner combustion chamber by using hydrogen fuel. Large Eddy Simulation (LES) was performed with the inner combustion chamber as shown in Fig.1 The time-averaged temperature field are shown in Fig.2. We confirmed the numerical analysis of exit gas temperature are consistent with the experimental results.

Annual Report Figures for 2024

Fig.1: Computational grid around injectors

 

Annual Report Figures for 2024

Fig.2: Time-averaged temperature field of inner combustion chamber

 

Publications

N/A

Usage of JSS

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: OpenMP
  • Number of Processes: 1 - 1534
  • Elapsed Time per Case: 240 Hour(s)

JSS3 Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.34

 

Details

Please refer to System Configuration of JSS3 for the system configuration and major specifications of JSS3.

Computational Resources
System Name CPU Resources Used
(Core x Hours)
Fraction of Usage*2(%)
TOKI-SORA 9019793.23 0.41
TOKI-ST 1582.17 0.00
TOKI-GP 0.00 0.00
TOKI-XM 0.00 0.00
TOKI-LM 0.00 0.00
TOKI-TST 0.00 0.00
TOKI-TGP 0.00 0.00
TOKI-TLM 0.00 0.00

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 31.22 0.02
/data and /data2 112715.11 0.54
/ssd 278.89 0.01

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 1.80 0.01

*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 Resources
ISV Software Licenses Used
(Hours)
Fraction of Usage*2(%)
ISV Software Licenses
(Total)
16.29 0.01

*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.

JAXA Supercomputer System Annual Report February 2024-January 2025