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Study on dynamic instability of a reentry capsule at transonic speed

JAXA Supercomputer System Annual Report February 2021-January 2022

Report Number: R21ETET12

Subject Category: Skills Acquisition System

PDF available here

  • Responsible Representative: Takashi Takahashi(Aeronautical Technology Directorate)
  • Contact Information: Yuya ohmichi (ohmichi.yuya@jaxa.jp)
  • Members: Masato Harafuji

Abstract

Atmospheric entry capsules are known to be prone to dynamic instabilities during subsonic to transonic speed flight.It has also been suggested that low-frequency fluid phenomena may have an effect on the dynamic instability. In this study, in order to better understand wake phenomena, numerical fluid simulations were performed on a normal flat plate to investigate the wake structure using dynamic mode decomposition.

Reference URL

N/A

Reasons and benefits of using JAXA Supercomputer System

Large computation cost to simulate unsteady flow fields.

Achievements of the Year

A DMD analysis was performed on the numerical results for a normal flat plate at M=0.2. Figure 1 shows the collapse of the spanwisel vortex at low frequencies obtained from the DMD. The wavelength of the collapse is shown in Figure 2, and the characteristic structure of the low-frequency fluid phenomenon can be found.

Annual Reoprt Figures for 2021

Fig.1: Vortex core structure behind a normal flat plate

 

Annual Reoprt Figures for 2021

Fig.2: Decay wavelength of vortex core

 

Publications

- Oral Presentations

M. Harafuji, Y. Ohmichi, M. Kanazaki, "Mode Decomposition Analysis for Low-Frequency Phenomenon of the Wake behind a Normal Flat Plate"AIAA SCITECH 2022 Forum, January 2022.

Usage of JSS

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: N/A
  • Number of Processes: 128 - 524
  • Elapsed Time per Case: 50 Hour(s)

JSS3 Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.04

 

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 769164.12 0.04
TOKI-ST 43897.03 0.05
TOKI-GP 0.00 0.00
TOKI-XM 0.00 0.00
TOKI-LM 11639.31 0.87
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 250.00 0.25
/data and /data2 44544.00 0.48
/ssd 50.00 0.01

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 28.77 0.19

*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)
365.00 0.26

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

JAXA Supercomputer System Annual Report February 2021-January 2022


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