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Research on combustor simulation

JAXA Supercomputer System Annual Report April 2017-March 2018

Report Number: R17ETET23

Subject Category: Skills Acquisition System

PDF available here

  • Responsible Representative: Takashi Aoyama, Aeronautical Technology Directorate, Numerical Simulation Research Unit
  • Contact Information: Rui Toyonaga toyonaga.l.0121@ruri.waseda.jp
  • Members: Rui Toyonaga

Abstract

For the development of a jet engine combustor with high environmental compatibility, we develop the combustion calculation code that can capture the pressure propagation and chemical reaction with practical calculation cost. In addition, a verification calculation of this calculation code is conducted on the scramjet test engine of DLR.

Reference URL

N/A

Reasons for using JSS2

It is necessary to use supercomputer to conduct development and verification of the combustion calculation code.

Achievements of the Year

In this research, the implementation of the combustion calculation code based on compressible flamelet model to a density- based fluid analysis solver, FaSTAR (FAST Aerodynamic Routines) was conducted. Then, an artificial neural network (ANN) model was applied to reduce the calculation cost when referring to the flamelet library. The ANN model has 2 input units (mixture fraction and scalar dissipation rate), 3 hidden units, and output units corresponding to mass fraction of each chemical species (As an example, Fig.1 shows the ANN model of OH mass fraction). In addition, we introduced the variance of the mixing fraction to the Flamelet library, which was conventionally obtained by mixing fraction and scalar dissipation rate. By this, the effect of turbulence of each species mass fraction was taken into account, and the precision of the Flamelet library has been improved (Fig2: Extension of the Flamelet library by the probability probability function method).

Annual Reoprt Figures for 2017

Fig.1: OH mass fraction generated by ANN

 

Annual Reoprt Figures for 2017

Fig.2: Extension of the Flamelet library by the probability probability function method

 

Publications

■ Non peer-reviewed papers

1) Rui Toyonaga, Himeko Yamamoto, Yasuhiro Mizobuchi, Tetsuya Sato, Numerical investigation on supersonic combustion in SCRAMJET engine by FaSTAR, JAXA Special Publication, 2017.12

2) Himeko Yamamoto, Rui Toyonaga, Yasuhiro Mizobuchi, Tetsuya Sato, Numerical analysis of jet lifted flames using G- equation, JAXA Special Publication, 2017.12

■ Presentations

1) Himeko Yamamoto, Rui Toyonaga, Yasuhiro Mizobuchi, Tetsuya Sato, Numerical study on flame structure of jet lifted flames by FaSTAR, 57th Aerospace Propulsion Conference of Japan Society for Aeronautical and Space Science, 2017.3

2) Himeko Yamamoto, Rui Toyonaga, Yasuhiro Mizobuchi, Tetsuya Sato, Numerical analysis of jet lifted flames using G- equation, 49th Fluid Dynamics Conference/ 35th Aerospace Numerical Simulation Symposium, 2017.6

3) Himeko Yamamoto, Rui Toyonaga, Yusuke Komatsu, Koki Kabayama, Yasuhiro Mizobuchi, Tetsuya Sato, Improvement of compressible flamelet model using artificial neural network, The Asian Joint Conference on Propulsion and Power, 2018.3

Usage of JSS2

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: N/A
  • Number of Processes: 2 - 1024
  • Elapsed Time per Case: 150.00 hours

Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.22

 

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 1,746,759.24 0.23
SORA-PP 980.73 0.01
SORA-LM 361.16 0.19
SORA-TPP 0.00 0.00

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 476.84 0.33
/data 9,765.63 0.18
/ltmp 1,953.13 0.15

 

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


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Language / 言語

"Annual Report" available

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

Location

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