分析滑动对马赫数 5 平板边界层波的稳定性和相互作用的影响

IF 1.1 4区工程技术 Q4 MECHANICS

International Journal of Computational Fluid Dynamics Pub Date : 2024-07-18 DOI:10.1080/10618562.2024.2376096

Lun Zhang, Zhongzheng Jiang, Hongwei Liu, Weifang Chen

引用次数: 0

摘要

高速飞机的边界层过渡与轻微稀释问题近来受到越来越多的关注。本文研究了高速飞行器在轻微稀释情况下边界层过渡的稳定性和共振相互作用。

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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Analysis of Slip Effects on the Stability and Interactions of Mach 5 Flat-Plate Boundary-Layer Waves

The issue of boundary-layer transition with slight rarefaction for high-speed aircraft has recently received increased attention. In this paper, the stability and resonant interactions of boundary-...

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来源期刊

International Journal of Computational Fluid Dynamics 物理-力学

CiteScore

2.70

自引率

7.70%

发文量

审稿时长

3 months

期刊介绍： The International Journal of Computational Fluid Dynamics publishes innovative CFD research, both fundamental and applied, with applications in a wide variety of fields. The Journal emphasizes accurate predictive tools for 3D flow analysis and design, and those promoting a deeper understanding of the physics of 3D fluid motion. Relevant and innovative practical and industrial 3D applications, as well as those of an interdisciplinary nature, are encouraged.