Research on Thermal Protection of Control Rudder Shaft of Hypersonic Vehicle
The control rudder is a key component for controlling the attitude of hypersonic aircraft, but the gap area of the rudder is prone to serious thermal load problems. This study adopted a novel control method for preventing aerodynamic heat, and through numerical simulation, the distribution law of ae...
Saved in:
| Main Authors: | Jiaqi QIN, Zhiwei SHI, Weilin ZHANG |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
China Astronautic Publishing CO., LTD. ; Editorial Office of Physics of Gases
2025-05-01
|
| Series: | 气体物理 |
| Subjects: | |
| Online Access: | http://qtwl.xml-journal.net/cn/article/doi/10.19527/j.cnki.2096-1642.1137 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Analysis of Aerothermal Environment Characteristics of Hypersonic Rudder Shaft Gaps
by: Zhiyi REN, et al.
Published: (2025-01-01) -
Numerical Simulation of Flow and Aerodynamic Heating of a Thermal-Protection Ring of Plate/Rudder Shaft
by: Yibin DOU, et al.
Published: (2024-11-01) -
Numerical Investigations and Optimized Design of the Active Cooling Performance with Phase Change for Aircraft Rudder Shaft
by: Xiangchun Sun, et al.
Published: (2025-07-01) -
Maneuverable unmanned aerial vehicle "rudder - drive” system design for aeroelastic stability
by: V. N. Akimov, et al.
Published: (2019-08-01) -
Investigation of the Asymmetric Features of X-Rudder Underwater Vehicle Vertical Maneuvring and Novel Motion Prediction Technology
by: Yinghua Li, et al.
Published: (2025-06-01)