[go: up one dir, main page]

Sekimoto et al., 2012 - Google Patents

Comparative study of co-flow and counter blowing DBD plasma actuators for separated flow over an airfoil

Sekimoto et al., 2012

Document ID
1815446007043437774
Author
Sekimoto S
Asada K
Anyoji M
Nonomura T
Fujii K
Publication year
Publication venue
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

External Links

Snippet

Some micro devices for active flow control, such as a synthetic jet or a single dielectric barrier discharge (DBD) plasma actuator (hereafter plasma actuator), are getting a lot of attentions because they can control separated flow with very small input energy and …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • Y02T50/16Drag reduction by influencing airflow
    • Y02T50/166Drag reduction by influencing airflow by influencing the boundary layer

Similar Documents

Publication Publication Date Title
Sidorenko et al. Pulsed discharge actuators for rectangular wing separation control
Zhang et al. Turbulent boundary layer separation control using plasma actuator at Reynolds number 2000000
Ruisi et al. Active flow control over a backward-facing step using plasma actuation
Liu et al. Aerodynamic control of NACA 0021 airfoil model with spark discharge plasma synthetic jets
WO2014084925A1 (en) Rail plasma actuator for high-authority flow control
Benard et al. Airflow reattachment along a NACA 0015 airfoil by surfaces dielectric barrier discharge actuator: Time-resolved particle image velocimetry investigation
Baleriola et al. Circulation control on a rounded trailing-edge wind turbine airfoil using plasma actuators
Ramakumar Flow control and lift enhancement using plasma actuators
Mack et al. Experimental investigation of separation and separation control on a laminar airfoil
Sekimoto et al. Comparative study of co-flow and counter blowing DBD plasma actuators for separated flow over an airfoil
Esfahani et al. Flow separation control over a Boeing Vertol VR-7 using NS-DBD plasma actuators
Mabe et al. Single dielectric barrier discharge plasma actuators for improved airfoil performance
Güler et al. Effect of signal modulation of DBD plasma actuator on flow control around NACA 0015
Engin et al. Large scale spanwise periodic vortex gusts or single spanwise vortex impinging on a rectangular wing
Leroy et al. Comparison of flow modification induced by plasma and fluidic jet actuators dedicated to circulation control around wind turbine airfoils
Pierre et al. Unsteady forcing of a post-stall flow over N NACA0012 airfoil by A surface DBD actuator
Schatzman et al. Turbulent boundary layer separation control using plasma actuators
Zheng Flow separation control over an airfoil using continuous alternating current plasma actuator
Sekimoto et al. Experimental study of a nano-second pulse plasma actuator for low reynolds number flow control
Sekimoto et al. Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation
Gejima et al. Suppression of vortex shedding from a pantograph head using vortex generator-type plasma actuators
Sirohi et al. Experimental characterization of the RailPAc plasma flow actuator
KC et al. Investigation of Wake Survey over a Wing with Conformal Vortex Generators
Sekimoto et al. Experimental study of burst ratio effect for dielectric-barrier-discharge plasma actuator for separation control
Zheng et al. Momentum transfer in millisecond periodic-pulsed dielectric-barrier-discharge plasma actuator