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Study of forward flight performance of multi-rotor

JAXA Supercomputer System Annual Report February 2021-January 2022

Report Number: R21ETET07

Subject Category: Skills Acquisition System

PDF available here

  • Responsible Representative: Yuto Sayama, Graduate student, Tokyo University of Agriculture and Techonology
  • Contact Information: Hideaki Sugawara(sugawara.hideaki@jaxa.jp)
  • Members: Yuto Sayama, Hideaki Sugawara, Yasutada Tanabe

Abstract

Study of forward flight performance of multi-rotor aircraft

Reference URL

N/A

Reasons and benefits of using JAXA Supercomputer System

In order to perform a rotorcraft analysis tool.

Achievements of the Year

Numerical analyses are performed on a rotor of a multi-rotor aircraft using rotorcraft CFD tool. To examine the advantages of a configuration with a propeller for propulsion and flying forward with a horizontal attitude (Fig. 1), the forward flight performance of the rotor was investigated by changing the forward tilt angle of the rotor. The results show that the smaller forward tilt angle improves the forward flight performance (Fig. 2).

Annual Reoprt Figures for 2021

Fig.1: Multi-rotor aircraft equipped with a propeller for propulsion and flying forward in a horizontal attitude.

 

Annual Reoprt Figures for 2021

Fig.2: Effective lift-to-drag ratio of a rotor relative to the rotor tilt angle. Effective lift-to-drag ratio is a index of the forward flight performance of a rotor.

 

Publications

- Non peer-reviewed papers

Sayama, Y., Hayami, K., Tanabe, Y., Sugawara, H., and Kameda, M., "PERFORMANCE OF A DUAL-CONTROLLED ROTOR IN LEVEL FLIGHT," 47th European Rotorcraft Forum, (2021).

- Oral Presentations

Sayama, Y., Hayami, K., Tanabe, Y., Sugawara, H., and Kameda, M., "PERFORMANCE OF A DUAL-CONTROLLED ROTOR IN LEVEL FLIGHT," 47th European Rotorcraft Forum, (2021).

Usage of JSS

Computational Information

  • Process Parallelization Methods: N/A
  • Thread Parallelization Methods: OpenMP
  • Number of Processes: 1
  • Elapsed Time per Case: 100 Hour(s)

JSS3 Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.02

 

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 0.00 0.00
TOKI-ST 162962.79 0.20
TOKI-GP 0.00 0.00
TOKI-XM 0.00 0.00
TOKI-LM 0.00 0.00
TOKI-TST 809.75 0.02
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 539.18 0.54
/data and /data2 33814.51 0.36
/ssd 500.99 0.13

 

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.

 

ISV Software Licenses Used

ISV Software Licenses Resources
ISV Software Licenses Used
(Hours)
Fraction of Usage*2(%)
ISV Software Licenses
(Total)
152.96 0.11

*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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"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