Preliminary evaluation of thrust loss in commercial aircraft engine due to airborne collision with Unmanned Aerial Vehicles (UAVs)

• المؤلفون الرئيسيون: Mohd Hasrizam Che Man, Liu, Hu, Ng, Bing Feng, Low, Kin Huat
• مؤلفون آخرون: 2020 International Conference on Unmanned Aircraft Systems (ICUAS)
• التنسيق: Conference or Workshop Item
• اللغة: English
• منشور في: 2021
• الموضوعات: Engineering::Aeronautical engineering::Accidents and air safety; Finite Element Method Simulation; Airborne Collision
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/148349
• المؤسسة: Nanyang Technological University

This paper is devoted to investigating the influence of UAVs airborne collision with civil aircraft engine on the operation safety of commercial aircraft. The damage levels of the civil aircraft fan blades and compressor blades during the UAVs airborne collision are both evaluated based on the Finit...