Research Article
Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow
Table 3
Comparison of aerodynamic effects on stress.
| | Without aerodynamic loads | Under aerodynamic force | Under aeroheating | | Surface temperature | Gas expansion |
| | Skin stress (MPa) | 4.4 | 28.4 | 27.0 | 6.7 | | Toroid stress (MPa) | 16.0 | 21.2 | 19.9 | 34.1 |
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