Fig. 4From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraftTemperature contours and correlation along with X at different y = 0.06, 0.26 and 0.46 between flow field and inner structure. a Hypersonic flow field, b Temperature correlation along with X, c Structural deformationBack to article page