带前体双三角翼气动特性研究

2021 8th International Conference on Signal Processing and Integrated Networks (SPIN) Pub Date : 2021-08-26 DOI:10.1109/SPIN52536.2021.9566062

Hrutvik Dhaigude, Vibhati, J. Sinha, J. K. Jain

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引用次数: 1

摘要

世界各地和生活的各个方面都在观察到技术的迅速发展。因此，军事部门对高效、机动和高速飞机的需求正在上升。三角翼是目前最明显的选择，许多杰出人士在这个领域已经投入了大量的工作。本文讨论了具有不同迎角前体的三角翼所具有的独特特性。设计了一种75/40结构的双三角翼，并将其与前体结合，以观察整个固体飞机的效果。本文通过模拟显示了流动分离、涡的产生、一次涡线和二次涡线，以了解气动特性和前体的影响。

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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Aerodynamic Characteristics of a Double Delta Wing with Fore-body

The brisk development in technology is being observed throughout the world and in every aspect of life. Thus, the demand for a highly efficient, maneuverable with high-speed aircraft is rising for the military sector. Delta wings are the most palpable choice right now and a lot of work has been devoted by many distinguished people in this area. This paper covers the unique characteristics exhibited by a delta wing with a forebody at various angles of attack. A Double Delta wing of 75/40 configuration has been designed and incorporated with a forebody to observe the effect of the whole solid aircraft. Flow separation, vortex generation, primary and secondary vortex lines have been shown through simulations to understand the aerodynamic characteristics and the effect of fore-body in this paper.

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来源期刊

2021 8th International Conference on Signal Processing and Integrated Networks (SPIN)

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