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首页> 外文期刊>Journal of Spacecraft and Rockets >Analytic Corrections to Computational Heating Predictions Accounting for Changes in Surface Catalysis
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Analytic Corrections to Computational Heating Predictions Accounting for Changes in Surface Catalysis

机译:考虑表面催化变化的计算加热预测的解析校正

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摘要

A new approach for combining the insight afforded by integral boundary-layer analysis with comprehensive (but time-intensive) computational fluid dynamic flowfield solutions of the thin-layer Navier-Stokes equations is described. The approach extracts computationally simulated quantities at the wall and at the boundary-layer edge for inclusion in a postprocessing boundary-layer analysis. It allows a designer at a workstation to address the question, given a single computational solution, "How much does the heating change for a thermal protection system with catalytic properties different from those used in the original numerical simulation?" Capabilities of this approach for application to reusable launch vehicle design are demonstrated. If the definition of surface catalysis is uncertain early in the design process, results show that fully catalytic wall boundary conditions provide the best baseline for computationally simulated design points.
机译:描述了一种将积分边界层分析提供的见解与薄层Navier-Stokes方程的全面(但费时)计算流体动力流场解决方案相结合的新方法。该方法提取墙和边界层边缘处的计算模拟量,以包含在后处理边界层分析中。有了一个单一的计算解决方案,它就可以使工作站的设计人员解决该问题:“具有催化特性的热保护系统的热变化与原始数值模拟所用的热变化有多少?”演示了这种方法在可重复使用运载火箭设计中的应用能力。如果在设计过程的早期不确定表面催化的定义,则结果表明完全催化的壁边界条件为计算模拟的设计点提供了最佳基准。

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