Flowfield prediction of a probe entering the Martian atmosphere

【Author】

Junming Lü;Qiang Wang;Xiaoli Cheng;

【Abstract】

<正>Based on the hypersonic entry in the Entry-Descending-Landing procedure,the three-dimensional Navier-Stokes equations are solved by a parallel code to analyze the flow field structures,aerodynamic characteristics and their variation patterns of the Mars Science Laboratory entering the Martian atmosphere with and

【Keywords】

As;Flowfield prediction of a probe entering the Martian atmosphere;

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