Fig. 7From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraftMacro-variables around Tiangong-type spacecraft with H = 90km, Ma∞ = 8 with thermodynamic non-equilibrium. a Translational Temp., b Rotational Temp., c Vibrational Temp., d Overall Temp., e Mach No., f Streamline structureBack to article page