Fig. 12From: Gas-kinetic unified algorithm for computable modeling of Boltzmann equation and application to aerothermodynamics for falling disintegration of uncontrolled Tiangong-No.1 spacecraftContours of number density, temperature, Mach number and streamlines past three side-by-side square cylinder for Kn∞ = 0.001, Ma∞ = 3 with spacing H = 6L. a Number density, b Temperature, c Mach number, d Flow streamlinesBack to article page