Effect of roll angle configurations of a reverse delta type add-on device on wing tip vortex alleviation

• Main Authors: Altaf, Afaq, Mohammed Aldheeb, Mohammed Abdulmalek, Omar, Ashraf Ali, Asrar, Waqar
• Format: Article
• Language: English; English
• Published: Semarak Ilmu Publishing 2024
• Subjects: TJ Mechanical engineering and machinery; TL500 Aeronautics
• Online Access: http://irep.iium.edu.my/118413/7/118413_%20Effect%20of%20roll%20angle%20configurations.pdf; http://irep.iium.edu.my/118413/8/118413_%20Effect%20of%20roll%20angle%20configurations_Scopus.pdf; http://irep.iium.edu.my/118413/; https://semarakilmu.com.my/journals/index.php/CFD_Letters/article/view/4630; https://doi.org/10.37934/cfdl.16.4.120133

An add-on device in the shape of a reverse delta has shown the ability to alleviate wake vortices. The present work studies the interaction of the wing tip vortex and the reverse delta type add-on device vortices. This paper looks at the vortex interactions generated downstream of the wing tip in pl...