Lift enhancement based on virtual aerodynamic shape using a dual synthetic jet actuator-Reference-Cited by-同舟云学术

Lift enhancement based on virtual aerodynamic shape using a dual synthetic jet actuator

Published:2022-12 Issue:12 Volume:35 Page:117-129
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Shiqing,LUO Zhenbing,DENG Xiong,LIU Zhiyong,GAO Tianxiang,ZHAO Zhijie

Funder

National Natural Science Foundation of China

National University of Defense Technology

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference23 articles.

1. Lift enhancement method by synthetic jet circulation control;Zhang;Sci China Technol Sci,2012

2. Test techniques for high lift two dimensional airfoil with boundary layer and circulation control for application to rotary wing aircraft;Englar;Can Aeronaut Space J,1973

3. 2-D Circulation control airfoil benchmark experiments intended for CFD code validation;Englar,2009

4. Advances in pneumatic-controlled high-lift systems through pulsed blowing;Jones,2003

5. An active flow circulation controlled flap concept for general aviation aircraft applications;Jones,2002

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