带有 Scramjet 入口内膨胀波干扰的 SWTBLI 湍流建模

IF 1.1 4区工程技术 Q4 MECHANICS

International Journal of Computational Fluid Dynamics Pub Date : 2023-12-27 DOI:10.1080/10618562.2023.2195642

Kavan M. Prabtani, Rajesh Ranjan

引用次数: 0

摘要

准确预测扰流式喷气发动机入口/隔离器内的流场对于稳定可靠的气动设计至关重要。然而，冲击波-膨胀波等复杂现象会对气动设计产生影响。

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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Turbulence Modelling for SWTBLI with Expansion Wave Interference Inside Scramjet Inlets

An accurate prediction of the flowfield inside the scramjet inlet/isolator is crucial for a stable and reliable aerodynamic design. However, the complex phenomena such as shock wave-expansion wave ...

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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.