Nanosecond Pulsed Plasma Actuation Effects on Aerodynamic Damping and Aeroelastic Stability Implications in the Post-Stall Regime-Reference-Cited by-同舟云学术

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Nanosecond Pulsed Plasma Actuation Effects on Aerodynamic Damping and Aeroelastic Stability Implications in the Post-Stall Regime

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
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Author:

Glaz Bryan,Dinavahi Surya,Gaitonde Datta

Publisher

American Institute of Aeronautics and Astronautics

Reference24 articles.

1. Compressible Dynamic Stall Performance of a Variable Droop Leading Edge Airfoil with a Gurney Flap

2. The control of flow separation by periodic excitation

3. Rotorcraft Aeromechanics: Getting through the Dip

4. A History of the Electric Wind

5. SDBD plasma enhanced aerodynamics: concepts, optimization and applications

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Large eddy simulation of dynamic stall flow control for wind turbine airfoil using plasma actuator;Energy;2020-12

2. Nanosecond Dielectric Barrier Discharge Plasma Actuator Flow Control of Compressible Dynamic Stall;46th AIAA Plasmadynamics and Lasers Conference;2015-06-18

3. A model for Nanosecond Pulsed Dielectric Barrier Discharge (NSDBD) actuator and its investigation on the mechanisms of separation control over an airfoil;Science China Technological Sciences;2013-03-16

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