Numerical investigation of splitter plate effect on the bluff body using finite volume method

• Main Authors: Abdul Aabid, Azmil Afifi, Khan, Sher Afghan
• Format: Conference or Workshop Item
• Language: English; English; English
• Published: Elsevier Ltd 2021
• Subjects: TL780 Rockets
• Online Access: http://irep.iium.edu.my/92649/7/92649_Numerical%20investigation%20of%20splitter%20plate%20effect%20on%20bluff.pdf; http://irep.iium.edu.my/92649/8/92649_Numerical%20investigation%20of%20splitter%20plate%20effect%20on%20bluff%20body_Scopus.pdf; http://irep.iium.edu.my/92649/19/92649_Numerical%20investigation%20of%20splitter%20plate_WoS.pdf; http://irep.iium.edu.my/92649/; https://www.journals.elsevier.com/materials-today-proceedings; https://doi.org/10.1016/j.matpr.2020.05.559

In an aerodynamics study, whenever there is a flat/blunt face, it will result in the maximum drag effect on the flat body. In these types of problems, the splitter plates have found a significant role in reducing the drag force. The splitter plate will separate/bifurcate the flow at the front face o...