Yüksek hızlı insansız hava aracı modellemesi ve simülasyonu

Unmanned Aerial Vehicles (UAVs) have appeared as a pivotal industry in contemporary times, attributed to their adeptness at executing intricate tasks in both civilian and military domains without endangered human lives. Consequently, numerous researchers have passionately studied these aircraft. Especially under stringent and challenging conditions, to ascertain their structural integrity post-manufacture. The focal point of this thesis is an in-depth analysis of the Boeing X-45C aircraft, with particular emphasis on its fuselage. The aircraft will be meticulously designed and rendered using the SOLIDWORKS software, adhering to its authentic dimensions. After this design phase, the aircraft will be positioned within a precisely defined fluidic environment to facilitate a comprehensive CFD simulation using the ANSYS Fluent software, simulating the aircraft's flight at peak velocities. This will be followed by an FSI simulation, intertwining the insights gleaned from the CFD analysis with the potential ramifications on the aircraft's aluminium structure. The culmination of the thesis will present a thorough commentary on the results, evaluating the success and efficacy of the simulations and analyses conducted. The findings underscored the robustness of the aircraft, confirming its resilience under the tested conditions. Keywords: FSI,