Analisis Aerodinamika Sayap Pesawat F-15 Ex Sebagai Air Carrier/ Pembawa Roket Peluncur Satelit Nano Dengan Menggunakan Metode Computational Fluid Dynamic (CFD)
DOI:
https://doi.org/10.54706/senastindo.v7.2025.425Keywords:
F-15 Ex Wing, Conputational Fluid Dynamic (CFD), Ansys SoftwareAbstract
This study aims to determine the aerodynamic characteristics of the F-15 Ex fighter jet wing before and after the installation of a nanosatellite launch rocket using the Computational Fluid Dynamic (CFD) method. The simulation was carried out using ANSYS software to analyze lift, drag, and aerodynamic coefficients (Cl, Cd, and L/D) at various angles of attack. The results show that a greater angle of attack produces higher lift, but also increases drag. At an angle of attack of 16°, the drag force reached 1842.356 N. These findings indicate that the F-15 Ex wing design with an attached rocket has potential as a nanosatellite launch carrier, provided aerodynamic efficiency and flight stability are maintained
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References
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