A series of calculations are carried out for a Mars Science Laboratory entry vehicle heat shield and compared with tests carried out in the Arnold Engineering Development Center for Mach 8 and 10 and a range of Reynolds numbers. Three turbulence models are employed that are implemented in the LAURA code: the Cebeci-Smith algebraic model, the 98 Wilcox k -^sUJ model, and the k -^sC, model. In general, good agreement is indicated with turbulent predictions. Because the flow is attached, the algebraic model performs as well as other models.
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机译：对于MARS科学实验室入口车辆隔热罩进行了一系列计算，并与马赫8和10的Arnold工程开发中心和一系列雷诺数进行了比较。采用三种湍流模型，其在劳拉码中实施：Cebeci-Smith代数模型，98 Wilcox K - ^ Suj模型，以及K - ^ Sc，模型。一般而言，湍流预测表明了良好的一致性。因为附加了流程，代数模型表现出以及其他模型。
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