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Structural analysis of Composite Fan blade

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17EA2720

Subject Category: Aeronautical Technology

PDF available here

  • Responsible Representative: Toshio Nishizawa, Aeronautical Technology Directorate, aFJR project team
  • Contact Information: Masahiro Hojo hojo.masahiro@jaxa.jp
  • Members: Masahiro Hojo, Kenshirou Kondou, Shota Sadamoto, Tomoaki Watanabe, Takuya Ando, Koji Miyazaki

Abstract

The purpose of aFJR project is to advance research on jet engine component technologies so that Japanese manufacturers can join more effectively in international joint-development projects on next-generation jet engines. The technology of the weight reduction of composite fan blade is researched in the aFJR project.

Reference URL

Please refer to 'aFJR (Advanced Fan Jet Research) project | ECAT - Environment-Conscious Aircraft Technology Program | Aeronautical Technology Directorate'.

Reasons for using JSS2

The hollow composite fan blade was designed based on the bird strike simulation results using JSS2.

Achievements of the Year

Figure 1 shows the analysis result of the bird strike simulation of hollow composite fan blade. The dynamic behavior of fan blade and the strain time histories were very close to those of the demonstration test result.

Annual Reoprt Figures for 2017

Fig.1: The bird strike simulation of hollow composite fan blade (a) t = 0.3 ms

 

Annual Reoprt Figures for 2017

Fig.2: The bird strike simulation of hollow composite fan blade (b) t = 0.9 ms

 

Annual Reoprt Figures for 2017

Fig.3: The bird strike simulation of hollow composite fan blade (c) t = 1.2 ms

 

Publications

N/A

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: OpenMP
  • Number of Processes: 128
  • Elapsed Time per Case: 50.00 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.20

 

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 1,364,797.48 0.18
SORA-PP 0.00 0.00
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 182.79 0.13
/data 56,745.24 1.05
/ltmp 5,533.86 0.42

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 6.93 0.29

*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