Aerodynamic Characteristics Improvement of Quad Tilt Wing VTOL Plane
JAXA Supercomputer System Annual Report April 2017-March 2018
Report Number: R17EA0901
Subject Category: Aeronautical Technology
- Responsible Representative: Shigeru Hamamoto, Aeronautical Technology Directorete, Aerodyamics Research Unit
- Contact Information: Yoshihisa Aoki aoki@chofu.jaxa.jp
- Members: Yoshihisa Aoki
Abstract
Improvement of aerodynamic characteristics of Quad Tilt Wing VTOL Plane in cruise.
Reference URL
N/A
Reasons for using JSS2
It takes a lot of time to calculate using workstation.
Achievements of the Year
Wing aspect ratio sensitivity analysis of practical demonstration unmanned plane was conducted using FaSTAR.
Publications
N/A
Usage of JSS2
Computational Information
- Process Parallelization Methods: MPI
- Thread Parallelization Methods: OpenMP
- Number of Processes: 160 – 640
- Elapsed Time per Case: 10.00 hours
Resources Used
Fraction of Usage in Total Resources*1(%): 0.01
Details
Please refer to System Configuration of JSS2 for the system configuration and major specifications of JSS2.
System Name | Amount of Core Time(core x hours) | Fraction of Usage*2(%) |
---|---|---|
SORA-MA | 23,331.00 | 0.00 |
SORA-PP | 3,136.13 | 0.04 |
SORA-LM | 3.67 | 0.00 |
SORA-TPP | 0.00 | 0.00 |
File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
---|---|---|
/home | 035.76 | 0.02 |
/data | 596.05 | 0.01 |
/ltmp | 244.14 | 0.02 |
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