Effects of plasma actuator on flow over an airfoil

• المؤلف الرئيسي: Ang, Edwin Wen Jun
• مؤلفون آخرون: Chan Weng Kong
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2015
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Aerodynamics; DRNTU::Engineering::Mechanical engineering::Fluid mechanics
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/64482
• المؤسسة: Nanyang Technological University

This project investigates the feasibility of using Nanosecond Pulse Dielectric Barrier Discharge Plasma Actuator (NS-DBD) to replace existing flow controlling devices. The advantages of NS-DBD include simpler in design, light weight, present no parasite drag and allows active control with zero react...