{"title":"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","authors":"Ritesh Srivastava, Roopak Baliyan, Vivek Kumar Patel","doi":"10.1007/s42401-024-00333-x","DOIUrl":null,"url":null,"abstract":"<div><p>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.</p></div>","PeriodicalId":36309,"journal":{"name":"Aerospace Systems","volume":"8 2","pages":"325 - 348"},"PeriodicalIF":0.0000,"publicationDate":"2024-12-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Effect of various angular outlets on mixing of swirling multi-annular jets in different expanded confinement\",\"authors\":\"Ritesh Srivastava, Roopak Baliyan, Vivek Kumar Patel\",\"doi\":\"10.1007/s42401-024-00333-x\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>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.</p></div>\",\"PeriodicalId\":36309,\"journal\":{\"name\":\"Aerospace Systems\",\"volume\":\"8 2\",\"pages\":\"325 - 348\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2024-12-16\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aerospace Systems\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s42401-024-00333-x\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"Earth and Planetary Sciences\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Systems","FirstCategoryId":"1085","ListUrlMain":"https://link.springer.com/article/10.1007/s42401-024-00333-x","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"Earth and Planetary Sciences","Score":null,"Total":0}
Effect of various angular outlets on mixing of swirling multi-annular jets in different expanded confinement
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.
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