Using alternating direction implicit NND scheme, the TLNS equations were solved under the assumption of perfect gas, and the space grids of complex wing-shape were generated by solving parabolic partial differential equations. Finally, the numerical simulation results of liftbody-type were shown under the conditions: M∞=8.0,α=20°.
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刘伟,刘君.数值模拟类升力体外形高超声速粘性绕流[J].国防科技大学学报,2000,22(5):12-14. LIU Wei, LIU Jun. Numerical Simulation of Hypersonic Viscous Flows Over Liftbody-Type Vehicle[J]. Journal of National University of Defense Technology,2000,22(5):12-14.