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Advances in Aerodynamics
Fig. 8 | Advances in Aerodynamics

Fig. 8

From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraft

Fig. 8

Pressure contours of flow field, temperature distribution and deformation of structure during the first disintegration of H = 250~90 km around Tiangong-1 spacecraft. a Pressure distr. of H = 250 km, b Struct. Temp. of H = 120 km, c Normal stress, d Struct. Temp. of H = 110 km, e Structural deformation of H = 100 km, f Deformation of H = 95 km, g StructuralTemp. of H = 90 km

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