利用单盘和双盘锥形钉减少抛物面鼻锥的空气阻力和发热量

IF 1.7 4区工程技术 Q3 MECHANICS

Numerical Heat Transfer Part B-Fundamentals Pub Date : 2024-08-05 DOI:10.1080/10407790.2024.2387266

Md Shamim Raza, Anil Kumar Prasad, Laljee Prasad, Ashish Narayan

引用次数: 0

摘要

这项数值研究探讨了在超音速飞行器的鼻子上使用气钉设计来减少阻力和热负荷的问题。各种配置，包括单半球形和双半球形鼻翼，都能有效减少阻力和热负荷。

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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Reducing aerodynamic drag and heat generation in parabolic nose cones using single and double-disc tapered spikes

This numerical study investigates the use of aerospike designs on the noses of supersonic vehicles to reduce drag and heat loads. Various configurations, including single and double hemispherical s...

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来源期刊

Numerical Heat Transfer Part B-Fundamentals 工程技术-力学

CiteScore

2.40

自引率

0.00%

发文量

审稿时长

2.8 months

期刊介绍： Published 12 times per year, Numerical Heat Transfer, Part B: Fundamentals addresses all aspects of the methodology for the numerical solution of problems in heat and mass transfer as well as fluid flow. The journal’s scope also encompasses modeling of complex physical phenomena that serves as a foundation for attaining numerical solutions, and includes numerical or experimental results that support methodology development. All submitted manuscripts are subject to initial appraisal by the Editor, and, if found suitable for further consideration, to peer review by independent, anonymous expert referees. The Editor reserves the right to reject without peer review any papers deemed unsuitable.