Fig. 5From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraftMacro-variables for cylinder flows of Kn∞ = 0.01, Ma∞ = 5 solved by GKUA comparing with DSMC. a Pressure, b Mach No., c Overall Temp., d Translational Temp., e Rotational Temp., f Vibrational TempBack to article page