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Straight-body-type-fuselage fighter cfd simulation
NoAI: This project, including models, simulations, images, and descriptions, may not be used within datasets, during the developmental process, or as inputs for generative AI tools.
About the Straight-Body-Type-Fuselage Fighter CFD Simulation Project
To explore the impact of using a fighter fuselage in the design of a fighter jet, which generates advantageous vortices for maneuverability, a computational fluid dynamics (CFD) approach is employed. The study involves simulating a model of a straight-body-type-fuselage (SBTF) fighter, utilizing the Q-criterion to analyze vortices and employing a logarithmic grid to emphasize the micro-gridding effect of the turbulent boundary layer. The results offer in-depth quantitative data on velocity, pressure, trajectory of the vortex core, and distribution of negative surface pressure on the wings. These findings provide valuable insights for enhancing performance, increasing lift, and improving the agility and maneuverability of future fighter jet designs. The images and data used here are adapted from the work of: Sutrisno Sutrisno, Deendarlianto Deendarlianto, Tri Agung Rohmat, Setyawan Bekti Wibowo, Sigit Iswahyudi in the article titled '[Vortex Dynamics Analysis of Straight-Body-Type-Fuselage Fighter Using CFD Simulation]' published in the journal [Journal of Aerospace Technology and Management]. The source of the these can be found at [Link to the Source: https://www.scielo.br/j/jatm/a/FzmRSMCX7ZjBqNTLnMDcpnh/?lang=en#] . The images and data are licensed under CC BY 4.0 [License Link: https://creativecommons.org/licenses/by/4.0/]."
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