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NUMERICAL SIMULATION FOR HYPERSONIC FLOW OF NONEQUILIBRIUM GASES AROUND THE APOLLO COMMAND MODULE[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(1): 8-22. doi: 10.6052/0459-1879-1996-1-1995-297
Citation: NUMERICAL SIMULATION FOR HYPERSONIC FLOW OF NONEQUILIBRIUM GASES AROUND THE APOLLO COMMAND MODULE[J]. Chinese Journal of Theoretical and Applied Mechanics, 1996, 28(1): 8-22. doi: 10.6052/0459-1879-1996-1-1995-297

NUMERICAL SIMULATION FOR HYPERSONIC FLOW OF NONEQUILIBRIUM GASES AROUND THE APOLLO COMMAND MODULE

doi: 10.6052/0459-1879-1996-1-1995-297
  • Publish Date: 1996-01-25
  • A hybrid flux splitting method is used to develop an implicit NND scheme which possesses good stability characteristics and high converging velocity. The hypersonic flows of the perfect gas and nonequilibrium gas around the Apollo Command Module are simulated with the method by solving the N-S equations. The numerical results agree with the experimental data satisfactorily. The flow structure in the leeside and wake is studied with the topological method.

     

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      沈阳化工大学材料科学与工程学院 沈阳 110142

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