Optimal design of propellers for compound helicopters
JAXA Supercomputer System Annual Report February 2023-January 2024
Report Number: R23EDA201C21
Subject Category: Aeronautical Technology
- Responsible Representative: Kanako Yasue, Aviation Technology Directorate, team leader, Aircraft Life-cycle Innovation Hub, Airmobility Digital Design Team
- Contact Information: Keita Kimura(kimura.keita@jaxa.jp)
- Members: Fumihiro Kajiwara, Keita Kimura, Masahiko Sugiura, Hideaki Sugawara, Ryo Takahashi, Yasutada Tanabe
Abstract
The objective of this study is to implement the optimal design of side and tail propellers for JAXA’s proposed compound helicopter. The shapes are optimized to meet the design target flight conditions, and performance evaluation is conducted in the process by CFD. The side propellers are designed to maintain hovering performance while satisfying the requirements of high-speed forward flight, and the tail propeller is designed to achieve twice the speed of a conventional helicopter. This fiscal year, we advanced our analysis based on Computational Fluid Dynamics (CFD) regarding the flow field around the designed propellers.
Reference URL
N/A
Reasons and benefits of using JAXA Supercomputer System
In the optimal design of propeller blades, it is necessary to conduct performance analysis of a large number of shapes within a set design variable space. In order to perform this concurrently, it is essential to utilize the computational power of a supercomputer.
Achievements of the Year
This fiscal year, we conducted visualization and analysis of the flow field as to side propeller operations, particularly focusing on the effects of interference with the main rotor. As an example, we introduce a case where CFD simulation has been carried out on the interference between the main rotor and side propeller during hovering condition.
Figure 1 illustrates the tip vortices of the main rotor and side propeller during hovering. In compound helicopters, the side propeller is positioned directly beneath the main rotor, so it is particularly affected by the downwash during hovering. The tip vortices generated by the side propeller can be seen moving diagonally downward from the propeller.
Figure 2 shows the vertical velocity distribution around the main rotor and side propeller during hovering. The color blue represents downward velocity, indicating a strong downwash from the main rotor. The rotating side propeller within the downwash introduces a swirl (rotational) component to the flow field, resulting in a complex flow pattern. In this state, the propeller experiences increased potential thrust due to the rotational speed of the blades and the downwash velocity acting on the blade elements.
Publications
– Peer-reviewed papers
K. Kimura, H. Sugawara., and Y. Tanabe, “Aerodynamic Interference between Main Rotor and Side Propellers of a Winged-type Compound Helicopter in Hover”, TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 66(5), 174-185.
– Oral Presentations
[1] K. Kimura, H. Sugawara, Y. Tanabe, “Wind Tunnel Testing of Propellers for a High-Speed Compound Helicopter,” 61th Aircraft Symposium, 1B12, Kokura, Japan, 2023.
[2] K. Kimura, Y. Tanabe, H. Sugawara, “Optimal Design of Side Propellers for a Winged Compound Helicopter,” 9th Asian/Australian Rotorcraft Forum, Nanjing, China, 2023.
Usage of JSS
Computational Information
- Process Parallelization Methods: N/A
- Thread Parallelization Methods: OpenMP
- Number of Processes: 1
- Elapsed Time per Case: 72 Hour(s)
JSS3 Resources Used
Fraction of Usage in Total Resources*1(%): 0.19
Details
Please refer to System Configuration of JSS3 for the system configuration and major specifications of JSS3.
System Name | CPU Resources Used(Core x Hours) | Fraction of Usage*2(%) |
---|---|---|
TOKI-SORA | 672254.71 | 0.03 |
TOKI-ST | 1313051.14 | 1.42 |
TOKI-GP | 0.00 | 0.00 |
TOKI-XM | 0.00 | 0.00 |
TOKI-LM | 0.00 | 0.00 |
TOKI-TST | 0.00 | 0.00 |
TOKI-TGP | 0.00 | 0.00 |
TOKI-TLM | 0.00 | 0.00 |
File System Name | Storage Assigned(GiB) | Fraction of Usage*2(%) |
---|---|---|
/home | 1282.32 | 1.06 |
/data and /data2 | 125892.40 | 0.78 |
/ssd | 31306.95 | 2.96 |
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 Used(Hours) | Fraction of Usage*2(%) | |
---|---|---|
ISV Software Licenses(Total) | 0.05 | 0.00 |
*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.
JAXA Supercomputer System Annual Report February 2023-January 2024