Effects of the fluidization modes on conveying characteristics in the powder fueled ramjets via a multiple state model of the dense powder flows

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Shilin Gao, Haibin Zhang, Bofeng Bai
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引用次数: 0

Abstract

As the core component of powder fueled ramjets, accurately characterizing the dense powder conveying behaviors is crucial for the design of powder feeding system and for achieving the ramjet's energy control and multi-mode operations. Limited by the testing approaches for dense powders, a modified two-fluid model (TFM), integrating μ(I) rheology theory and Hooke’s law, has been constructed in this paper to depict the multiple states and nonlinear evolutions of dense granular flows within the powder feeding systems. And a piston dynamic mesh boundary, consistent with the actual process, was constructed. By using the modified TFM, the effects of fluidization modes on conveying characteristics were explored, revealing the nonlinear correlation between the powder rheological properties and the fluctuation of output flow rate. Furthermore, the impacts of fluidizing gas injection direction and the contraction angle of the storage tank on the conveying performance were investigated. The findings have indicated that the gas cavitation instability led to flow rate fluctuations, while reducing the contraction angle of the storage tank enhanced the output flow rate and solid-gas ratio. This study provides a novel approach and valuable insights for the designing propellant feeding systems, contributing significantly to the development of stable and controllable powdered fuel feeding technology for powder fueled ramjets.
基于致密粉末流多态模型的流化方式对粉末燃料冲压发动机输送特性的影响
作为粉末燃料冲压发动机的核心部件,致密粉末输送特性的准确表征对于给粉系统的设计、实现冲压发动机的能量控制和多模式运行至关重要。受致密粉体测试方法的限制,本文结合μ(I)流变理论和胡克定律,建立了一种改进的双流体模型(TFM)来描述致密颗粒流在给粉系统中的多态和非线性演化。建立了符合实际工艺的活塞动态网格边界。利用改进的TFM,探讨了流化方式对输送特性的影响,揭示了粉体流变性能与输出流量波动之间的非线性关系。进一步研究了流化气体注入方向和储罐收缩角对输送性能的影响。研究结果表明,气体空化不稳定性导致流量波动,而减小储罐收缩角可提高输出流量和固气比。该研究为推进剂进料系统的设计提供了新的思路和有价值的见解,对研制稳定可控的粉末燃料冲压发动机进料技术具有重要意义。
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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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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