Numerical Simulation of Hypersonic Viscous Flows Over Liftbody-Type Vehicle
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    Abstract:

    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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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.

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History
  • Received:October 30,1999
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  • Online: November 18,2013
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