{"title":"Improvement in aerodynamic efficiency of trainer aircraft wing using co flow jet method","authors":"J. Anish, G. M. Joselin Herbert, K. Balaji","doi":"10.1007/s42401-023-00256-z","DOIUrl":null,"url":null,"abstract":"<div><p>The objective of this paper is to enhance the aerodynamic performance of trainer aircraft wing using active flow control method of co flow jet (CFJ). In this numerical study, free stream velocity of 20 m/s and k epsilon turbulence model is used to compare baseline and CFJ aerofoils with different angles of attack (AOA). This work introduced CFJ method into the trainer aircraft wing to improve the aerodynamic performance by controlling the boundary layer over it at different AOA and at the same time to reduce the take-off landing distance. The obtained results show that the stalling AOA improved by 40% and lift coefficient increased by 52%. The same method could be used to all trainer aircrafts.</p></div>","PeriodicalId":36309,"journal":{"name":"Aerospace Systems","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2023-12-01","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/s42401-023-00256-z","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"Earth and Planetary Sciences","Score":null,"Total":0}
引用次数: 0
Abstract
The objective of this paper is to enhance the aerodynamic performance of trainer aircraft wing using active flow control method of co flow jet (CFJ). In this numerical study, free stream velocity of 20 m/s and k epsilon turbulence model is used to compare baseline and CFJ aerofoils with different angles of attack (AOA). This work introduced CFJ method into the trainer aircraft wing to improve the aerodynamic performance by controlling the boundary layer over it at different AOA and at the same time to reduce the take-off landing distance. The obtained results show that the stalling AOA improved by 40% and lift coefficient increased by 52%. The same method could be used to all trainer aircrafts.
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
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
