Effectiveness of micro synthetic jet actuator enhanced by flow instability in controlling laminar separation caused by adverse pressure gradient-Reference-Cited by-同舟云学术

Effectiveness of micro synthetic jet actuator enhanced by flow instability in controlling laminar separation caused by adverse pressure gradient

Published:2006-11 Issue:2 Volume:132 Page:607-615
ISSN:0924-4247
Container-title:Sensors and Actuators A: Physical
language:en
Short-container-title:Sensors and Actuators A: Physical

Author:

Hong Guang

Publisher

Elsevier BV

Subject

Electrical and Electronic Engineering,Metals and Alloys,Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation,Electronic, Optical and Magnetic Materials

Reference22 articles.

1. Role of actuation frequency in controlled flow attachment over a stalled airfoil;Amitay;AIAA J.,2002

2. Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators;Amitay;AIAA J.,2001

3. The evolution of round zero-net-mass-flux jets;Cater;J. Fluid Mech.,2002

4. Perturbed interaction between vortex shedding and induced vibration;Cheng;J. Fluids Struct.,2003

5. Flow Control, Passive, Active and Reactive Flow Management;Gad-el-Hak,2000

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