Numerical Simulation on Computational Model of Hypersonic Slip Flow

Three main computational models in hypersonic slip flow are derived and analyzed in detail and then compared by numerical simulation in which 2D cylinder hypersonic slip flow with Mach number 10 and Knudsen number 0.002, 0.01, 0.05, 0.25 are examined, results come out that the improved Maxwell slip model shows better applicability.