Load tests and moments evaluation of aircraft pylon using refurbished test assembly

• المؤلف الرئيسي: Subas Chandrabose Satheesh Kumar
• مؤلفون آخرون: Sunil Chandrakant Joshi
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2015
• الموضوعات: DRNTU::Engineering::Aeronautical engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/65168

An aircraft pylon is a suspension device under the fuselage or wing of an aircraft used to attach and carry missiles, gun pods, propulsion units, fuel tanks etc. The component-loaded pylon experiences considerable loads in yaw, pitch and roll during the corresponding aircraft flight manoeuv...