Study on combustor in mini jet engine

• المؤلف الرئيسي: Gao, Xuan
• مؤلفون آخرون: Fei Duan
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2013
• الموضوعات: DRNTU::Engineering::Mechanical engineering::Motors, engines and turbines
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/54552

Mini turbojet engines can be widely used for unmanned aerial vehicles due to their main advantages of small size and relatively high propulsion. This study focuses on the reverse flow combustor in the mini jet engine. It mainly includes the experiments and numerical simulation. The experiments have...