Effect of various angular outlets on mixing of swirling multi-annular jets in different expanded confinement

Q3 Earth and Planetary Sciences
Ritesh Srivastava, Roopak Baliyan, Vivek Kumar Patel
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引用次数: 0

Abstract

Multi-annular jets are derived from coaxial jets, which are used to improve the mixing of fuel and air before ignition in a gas turbine combustor and it is essential to achieving stable and effective combustion. In the present work, a multi-annular jet comprising two co-annular and one central jet has been used to understand the flow characteristics and mixing of jets in non-expanded and expanded confinement with different angular outlets. A computational investigation has been performed with different swirl combinations in three air jets inlet under non-combustion conditions. After validation from existing experimental results, parametric studies have been investigated with different expansion ratios, different swirl combinations, and different angular outlets. Using the realizable k–ε turbulence model and commercial software ANSYS FLUENT, results were obtained in the form of streamlines plots, axial velocity contours, and center line axial velocity. Following a comprehensive analysis of the computational output, it is found the mixing process in confinement depends on expansion ratios, swirl combinations, and angular outlets. Results show that the mixing of jets is enhanced in expanded confinement at particular swirl combinations and at certain angular outlets.

Abstract Image

不同角度出口对不同膨胀约束下旋流多环射流混合的影响
多环射流是由同轴射流发展而来的,用于改善燃气轮机燃烧室点火前燃料和空气的混合,是实现稳定有效燃烧的关键。本文采用由两个共环射流和一个中心射流组成的多环射流,研究了不同角度出口的非膨胀约束和膨胀约束中射流的流动特性和混合情况。在非燃烧条件下,对三种进气道的不同涡流组合进行了计算研究。在对已有实验结果进行验证的基础上,对不同膨胀比、不同旋流组合和不同角度出口进行了参数化研究。利用可实现的k -ε湍流模型和商业软件ANSYS FLUENT,以流线图、轴向速度轮廓和中心线轴向速度的形式获得了结果。通过对计算输出的综合分析,发现约束下的混合过程取决于膨胀比、旋流组合和角出口。结果表明,在特定的旋流组合和一定角度的出口下,射流的混合在扩展约束中得到增强。
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来源期刊
Aerospace Systems
Aerospace Systems Social Sciences-Social Sciences (miscellaneous)
CiteScore
1.80
自引率
0.00%
发文量
53
期刊介绍: Aerospace Systems provides an international, peer-reviewed forum which focuses on system-level research and development regarding aeronautics and astronautics. The journal emphasizes the unique role and increasing importance of informatics on aerospace. It fills a gap in current publishing coverage from outer space vehicles to atmospheric vehicles by highlighting interdisciplinary science, technology and engineering. Potential topics include, but are not limited to: Trans-space vehicle systems design and integration Air vehicle systems Space vehicle systems Near-space vehicle systems Aerospace robotics and unmanned system Communication, navigation and surveillance Aerodynamics and aircraft design Dynamics and control Aerospace propulsion Avionics system Opto-electronic system Air traffic management Earth observation Deep space exploration Bionic micro-aircraft/spacecraft Intelligent sensing and Information fusion
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