不同初始参数对煤油/空气两相旋转爆震发动机工作特性的影响

IF 6.4 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-06-01 Epub Date: 2025-03-01 DOI:10.1016/j.ast.2025.110117
Xiafei Li , Jianzhong Li , Wu Jin , Qian Yao , Qiongyao Qin , Li Yuan
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引用次数: 0

摘要

设计了一种基于高速剪切气流和燃油喷射的环形旋转爆震发动机(RDE)。对其爆轰燃烧特性进行了实验研究。在低出口收缩比下,RDE主要以“单爆震模式”工作;随着出口收缩比的增大,RDE呈现“复杂混合爆轰模式”。根据爆轰波速度和动压特性,发现“复杂混合爆轰模式”由“随机爆轰波”(0 ~ 1000m /s)、“单爆轰波”(1000 ~ 2000m /s)和“双爆轰波”(2000 ~ 4000m /s)组成。数值模拟和高频动压试验结果表明,“随机爆震波”模式下爆轰能量最弱,传播稳定性最差,“双爆震波”模式次之,“单爆震波”模式表现最佳。随后,提出了“复杂混合爆轰模式”下旋转爆震波的相关工作性能参数。进一步研究了不同进气总温度、当量比和空气质量流量对两相煤油/空气RDE波动特性和运行性能的影响。结果表明,不同的“爆震波”对RDE整体爆轰性能的贡献随初始参数的不同而不同,“双爆震波”的贡献随三组初始参数的增大而增大。此外,在最佳的进气总温度、等效比和空气流量参数下,RDE表现出最佳的性能和稳定性。在最优条件下,爆轰波速达到1531.5 m/s,波速标准差为14.62%。
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The influence of different initial parameters on the operational characteristics of a Kerosene/air two-phase rotating detonation engine
An annular rotating detonation engine (RDE) with an integrated fuel atomization and mixing structure based on high-speed shear air flow rate and fuel injection was designed for air/kerosene reactants. Experimental studies were conducted on its detonation combustion characteristics. Under a low outlet contraction ratio, the RDE primarily operated in a "Single Detonation Mode"; as the outlet contraction ratio increased, the RDE exhibited a "Complex Hybrid Detonation Mode." Based on detonation wave velocities and dynamic pressure characteristics, it was found that the "Complex Hybrid Detonation Mode" consists of "Random Detonation Wave" (0–1000 m/s), "Single Detonation Wave" (1000–2000 m/s), and "Double Detonation Wave" (2000–4000 m/s). Numerical simulations and high-frequency dynamic pressure test results indicate that the detonation energy is weakest and propagation stability poorest in the "Random Detonation Wave" mode, followed by the "Double Detonation Wave" mode, with the "Single Detonation Wave" mode demonstrating the best performance. Subsequently, relevant operational performance parameters of the rotating detonation wave for the "Complex Hybrid Detonation Mode" were proposed. The effects of varying total inlet air temperature, equivalence ratio, and air mass flow rate on the wave characteristics and operational performance of the two-phase kerosene/air RDE were further investigated. Results indicate that the contribution of different "Detonation wave" to the overall RDE detonation performance varies with different initial parameters, with the contribution of the "Double Detonation Wave" increasing with the rise in the three sets of initial parameters. Furthermore, optimal total inlet air temperature, equivalence ratio, and air flow rate parameters exist for which the RDE exhibits the best performance and stability. Under optimal conditions, the detonation wave velocity reached 1531.5 m/s, with a wave velocity standard deviation of 14.62 %.
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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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