Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow
The inflatable reentry vehicle provides a new technical way in aerospace entry, descent, and landing. The structural failure of inflatable reentry vehicle experiment caused by thermal aeroelastic effect is serious, which needs to be further studied. A traditional numerical method about flexible vehi...
Saved in:
| Main Authors: | Jie Wu, Zhang Zhang, Anping Hou, Xiaopeng Xue, Xu Cao |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2021-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2021/6673818 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Backward Scattering Characteristics of a Reentry Vehicle Enveloped by a Hypersonic Flow Field
by: Haoyu Sun, et al.
Published: (2018-01-01) -
Analysis of Aerodynamic Heating Modes in Thermochemical Nonequilibrium Flow for Hypersonic Reentry
by: Shuai He, et al.
Published: (2025-06-01) -
Multidisciplinary Design Optimization of Reentry-Powered Hypersonic Vehicles Based on Surrogate Model
by: Shoudong Ma, et al.
Published: (2024-01-01) -
A Closed-loop Optimal Feedback Guidance Method of Reentry Phase for Hypersonic Glide Vehicle
by: LIAO Yuxin, et al.
Published: (2018-01-01) -
Coordinated Reentry Guidance with A* and Deep Reinforcement Learning for Hypersonic Morphing Vehicles Under Multiple No-Fly Zones
by: Cunyu Bao, et al.
Published: (2025-06-01)