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Development of CFD technology to support design of aircraft combustor with real configuration.

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17EA2117

Subject Category: Aeronautical Technology

PDF available here

  • Responsible Representative: Takashi Yamane, Aeronautical Technology Directorate, Propulsion Research Unit
  • Contact Information: Mitsumasa Makida makida.mitsumasa@jaxa.jp
  • Members: Mitsumasa Makida(JAXA), Naoki Nakamura(ASIRI)

Abstract

In this research, we aim to obtain design methods for development of aircraft combustors with real configuration, which estimate dispersion of the fuel droplets, evaporation, and combustion processes.

Reference URL

N/A

Reasons for using JSS2

It is important to do parametric case study with slightly different geometry, and each case with spray and combustion needs large scale simulation. To conduct such simulation and visualization effectively, we use the super computer with high parallelization efficiency.

Achievements of the Year

In this fiscal year, we integrate real gas effect, fuel evaporation and chemical reaction model into the base solver, which enabled to simulate the distribution of fuel spray, fuel vapor and chemical reaction rate near the fuel nozzle with realistically complicated configuration.

Annual Reoprt Figures for 2017

Fig.1: Disrtibution of fuel spray, fuel vapor and reaction rate near fuel nozzle

 

Publications

N/A

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: Automatic Parallelizatio
  • Number of Processes: 120
  • Elapsed Time per Case: 300.00 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.31

 

Details

Please refer to System Configuration of JSS2 for the system configuration and major specifications of JSS2.

Computational Resources
System Name Amount of Core Time
(core x hours)
Fraction of Usage*2(%)
SORA-MA 2,536,622.63 0.33
SORA-PP 4,300.70 0.05
SORA-LM 0.00 0.00
SORA-TPP 0.00 0.00

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 211.66 0.15
/data 9,391.05 0.17
/ltmp 1,519.10 0.11

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 0.14 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.

JAXA Supercomputer System Annual Report April 2017-March 2018


ここは、サイドバー・エリアの先頭です。

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Language / 言語

"Annual Report" available

How to use JSS3

To use JSS3, please refer to "How to use JSS3" page .

Location

Chofu Aerospace Center
7-44-1 Jindaiji Higashi-machi, Chofu-shi, Tokyo