进气口直径对铝基喷水发动机流动结构和性能的影响

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Wei Xu, WenChun Bao, Zhe Fang, Yuntian Zhang, Yuanshu Liu, Guo-Yu Ding, PingHua Yan, ChaoQi Xu
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引用次数: 0

摘要

摘要 本研究通过数值模拟分析了铝基水流冲压喷射器的流场和性能。蒸发吸热过程中时间的减少扩大了铝/水的燃烧范围,增加了比冲。如果初级入口雾化水滴的直径较大,蒸发效率将进一步降低,不利于反应的进一步扩散。但如果直径较小,流场温度会因快速蒸发而急剧下降,燃烧器反应区会出现大范围的低温区。二次进水雾化水滴直径的减小,有利于向下游反应区扩散,进一步使燃烧范围扩大。这种效应有利于提高比冲,并可降低壁附近的温度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effect of inlet diameter on the flow structure and performance for aluminum-based water-jet engine
Abstract In this study, the flow field and performance for the aluminum based water ramjet was analyzed through numerical simulation. The time decrease in evaporation heat absorption process expands the range of aluminum/water combustion and increase the specific impulse. If the diameter of atomized water droplets from the primary inlet is large, the evaporation efficiency will be further reduced, which is not conducive to the further propagation of the reaction. However, if the diameter is small, the flow field temperature will be rapidly dropped due to rapid evaporation, and a large range of low-temperature areas will appear in the reaction area of the combustor. The diameter reduction of atomized water droplets from the secondary water inlet is conducive to the diffusion of the reaction area downstream, further and makes the combustion range be expanded. This effect is benefit for increasing the specific impulse and can reduce the temperature near the wall.
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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