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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Fig 9
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Research Article
Thermal Aeroelastic Characteristics of Inflatable Reentry Vehicle Experiment (IRVE) in Hypersonic Flow
Figure 9
Flow comparison between
Ma
12 and
Ma
5: (a, b) surface pressure; (c) streamline.
(a)
(b)
(c)