Fig. 6From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraftSurface pressure and heat flux for cylinder flows of Kn∞ = 0.01, Ma∞ = 5 solved by GKUA comparing with DSMC results with different non-equilibrium effects with the Shakhov model of simple gas, the ES model of rotational excitation polyatomic gas and the Nitrogen vibrational energy excitation, respectively. a Pressure, b Enlarged near stagnation point for pressure, c Heat flux, d Enlarged near stagnation point for heat fluxBack to article page