HALO3D：高超音速飞行模拟的全机械方法，第二部分

IF 1.1 4区工程技术 Q4 MECHANICS

International Journal of Computational Fluid Dynamics Pub Date : 2024-02-22 DOI:10.1080/10618562.2024.2306946

Shrutakeerti Mallikarjun, Vincent Casseau, Gan Yang, John Y. Huang, Wagdi G. Habashi, Song Gao, Abolfazl Karchani

引用次数: 0

摘要

本文是两篇系列论文 "HALO3D：HALO3D: An All-Mach Approach to Hypersonic Flows Simulation "系列论文的第二部分，介绍了用于高速飞行器设计的单片流动模拟软件的进展。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

HALO3D: An All-Mach Approach to Hypersonic Flows Simulation, Part II

This paper is Part II of the two-paper series ‘HALO3D: An All-Mach Approach to Hypersonic Flows Simulation’ presenting advances in a monolithic flow simulation software for the design of high-speed...

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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.