本文へ移動

サイトナビゲーションへ移動

検索ボックスへ移動

サイドバーへ移動

ここは、本文エリアの先頭です。

Research on high load compressor technology

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17EA0711

Subject Category: Aeronautical Technology

PDF available here

  • Responsible Representative: Toshiya Nakamura, Next Generation Aeronautical Innovation Hub Center
  • Contact Information: Junichi Kazawa kazawa.junichi@jaxa.jp
  • Members: Junichi Kazawa, Yuntae Lee, Takafumi Kanayama

Abstract

For the international joint development of jet engines, it aims to develop and demonstrate core engine technology with little experience in Japan. In order to achieve high aerodynamic performance of a compact size and a total pressure ratio of 20 or more, we designed a multi-stage axial compressor with mixed flow compressor applied in the final stage and confirmed its validity by numerical analyses.

Reference URL

Please refer to 'Green engine technology | ECAT - Environment-Conscious Aircraft Technology Program | Aeronautical Technology Directorate'.

Reasons for using JSS2

In multistage compressor analyses, the number of grid points is large. It is necessary to analyze many cases to obtain a performance curve. It is necessary to use supercomputers in order to produce results in a limited time period and feed back to the multistage compressor design.

Achievements of the Year

The aerodynamic performance was predicted by multi-stage steady-state analysis for the high pressure compressor with seven stage axial compressor and one mixed flow compressor designed by JAXA. Although there was a problem with aerodynamic performance in the initial design shape, we confirmed that it was improved by the improved design and confirmed the validity of the high pressure comressor design.

Annual Reoprt Figures for 2017

Fig.1: High Pressure Compressor (Designed by JAXA)

 

Annual Reoprt Figures for 2017

Fig.2: Improved design result (total pressure distribution)

 

Publications

N/A

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: OpenMP
  • Number of Processes: 66 - 95
  • Elapsed Time per Case: 5.50 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.21

 

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 1,482,092.70 0.19
SORA-PP 48,319.33 0.60
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 019.75 0.01
/data 197.55 0.00
/ltmp 4,045.76 0.31

 

Archiver Resources
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.

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。

News - Recent Posts

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