Effects of plasma actuator on flow over an airfoil

Effects of plasma actuator on flow over an airfoil

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...

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Bibliographic Details
Main Author: Ang, Edwin Wen Jun
Other Authors: Chan Weng Kong
Format: Final Year Project (FYP)
Language:English
Published: 2015
Subjects:
DRNTU::Engineering::Aeronautical engineering::Aerodynamics
DRNTU::Engineering::Mechanical engineering::Fluid mechanics
Online Access:http://hdl.handle.net/10356/64482

Internet

http://hdl.handle.net/10356/64482

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