Investigations on the initiation characteristics of radical-assisted oblique detonation waves generated by plasma discharges

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-08 DOI:10.1016/j.ast.2024.109466
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Abstract

The oblique detonation engine (ODE) faces issues such as no-ignition, difficulty in combustion, and unstable combustion, some proactive auxiliary ignition measures should be implemented. This paper explores the application of radical-assisted combustion technology in the ODE and studies the effects of radicals on the oblique detonation wave (ODW) initiation characteristics. The two-dimensional Navier-Stokes equations which take into account the elementary reaction of acetylene/ethylene-air mixtures are solved, including chain reaction initiation, branching, and termination. The results demonstrate that the addition of radicals yields significant improvements in accelerating the initiation of ODW. The introduction of H, O, or OH radicals decrease the characteristic length of the induction zone with the mole fraction increases. Conversely, the inclusion of CHO radicals leads to an increase in the characteristic length of the induction zone with increasing mole fraction, primarily due to dominant chemical reaction kinetic effects. Additionally, the paper conducts an ignition sensitivity analysis of the radicals on the chemical reaction mechanisms and their influence on the initiation characteristics. Finally, a comprehensive analysis is performed by comparing the numerical results with the constant volume combustion theory, focusing on two initiation patterns: wave-controlled and chemical kinetics-controlled configurations. It is observed that varying the particle parameters results in changing the boundary lines between these two initiation patterns, and increasing the mole fraction shifts the initiation pattern from wave-controlled to chemical kinetics-controlled.

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等离子体放电产生的激波辅助斜向起爆波的起爆特性研究
斜爆发动机(ODE)面临着不点火、燃烧困难、燃烧不稳定等问题,应采取一些积极的辅助点火措施。本文探讨了激元辅助燃烧技术在 ODE 中的应用,并研究了激元对斜向爆轰波(ODW)起爆特性的影响。本文求解了考虑乙炔/乙烯-空气混合物基本反应的二维纳维-斯托克斯方程,包括链式反应的起始、分支和终止。结果表明,加入自由基可显著改善 ODW 的启动速度。随着摩尔分数的增加,引入 H、O 或 OH 自由基会减少诱导区的特征长度。相反,加入 CHO 自由基会导致诱导区的特征长度随着摩尔分数的增加而增加,这主要是由于占主导地位的化学反应动力学效应。此外,本文还分析了自由基对化学反应机理的点火敏感性及其对引发特性的影响。最后,通过将数值结果与恒定体积燃烧理论进行比较,重点对两种起燃模式进行了综合分析:波控制和化学动力学控制构型。研究发现,改变颗粒参数会导致这两种起燃模式之间的边界线发生变化,而增加分子分数则会使起燃模式从波控模式转变为化学动力学控制模式。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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