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...
Main Authors: | Jie Wu, Zhang Zhang, Anping Hou, Xiaopeng Xue, Xu Cao |
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Format: | Article |
Language: | English |
Published: |
Hindawi Limited
2021-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/6673818 |
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