The three dimensional hypersonic viscous flow of perfect gas over a capsule is calculated numerically. The Navier-Stokes equations are taken as the governing equations. The implicit NND scheme is used for the shock capture. The computation region is involved with the full flowfíeld from the nose to the base. The flowfield properties and the areodynamic force coefficients thus obtained are good compared with the experiment results.
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柳军,瞿章华.再入飞行器高超声速三维粘性流场的数值模拟[J].国防科技大学学报,1996,18(2):1-4. Liu Jun, Qu Zhanghua. Numerical Simulation of 3-D Hypersonic Viscous Flowfield over a Capsule[J]. Journal of National University of Defense Technology,1996,18(2):1-4.