高超声速流动中穗根射流方向对阻力和减热的影响

Proceedings of the 2nd International Conference on Artificial Intelligence and Advanced Manufacture Pub Date : 2020-10-15 DOI:10.1145/3421766.3421886

Kun Ma, Yingkun Li, Liang Zhu

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引用次数: 0

摘要

刺根射流装置因其优异的热防护性能而受到世界各国的关注。本文研究了刺根射流方向对高超声速流动结构的影响及热防护效应。新模型的一小部分修正了纳维尔·斯托克斯方程和通过偏心进行的愚蠢转移。结果表明，在总质量流量和射流位置相同的情况下，射流方向对射流结构和热防护性能有影响。对向射流减阻性能最好，斜向射流防热效果最好。但相对于对向射流和斜向射流，侧向射流的减阻和减热性能最差。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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The Effect of the Spike Root Jet Direction on Drag and Heat Reduction in Hypersonic Flows

The device of the spike root jet gets worldwide attention due to its excellent performance on thermal protection. In this paper, the impression of the direction of the spike root jet on hypersonic flow structures and thermal protection affection has been studied. A small part of the new model to fix Navier Stokes'equation and the silly transfer through eccentricity has been developed. The results shows, with the same total mass flow rate and jet position, the jet direction has an influence on the flow structures and the thermal protection performance. The opposing jet has the best drag reduction performance and the oblique jet has the best thermal protection effect. However, compared with the opposing jet and oblique jet, the lateral jet has the worst performance on both drag and heat reduction.

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Proceedings of the 2nd International Conference on Artificial Intelligence and Advanced Manufacture

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