[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Sekimoto et al., 2016 - Google Patents

Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation

Sekimoto et al., 2016

Document ID
2025090857729294908
Author
Sekimoto S
Nonomura T
Fujii K
Publication year
Publication venue
54th AIAA Aerospace Sciences Meeting

External Links

Snippet

This study focuses on the multiple separation-control mechanisms of burst actuation with a dielectric barrier discharge plasma actuator. Control of separated flow around a NACA 0015 airfoil at the Reynolds number 63,000 is investigated with a plasma actuator mounted at 5 …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • Y02T50/166—Drag reduction by influencing airflow by influencing the boundary layer
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • Y02T50/162—Wing tip vortex reduction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/12—Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow

Similar Documents

Publication Publication Date Title
Feng et al. Flow control over an airfoil using virtual Gurney flaps
Zhang et al. Turbulent boundary layer separation control using plasma actuator at Reynolds number 2000000
Mohammadi et al. Active flow control by dielectric barrier discharge to increase stall angle of a NACA0012 airfoil
Ebrahimi et al. Experimental study of stall control over an airfoil with dual excitation of separated shear layers
Benard et al. Airflow reattachment along a NACA 0015 airfoil by surfaces dielectric barrier discharge actuator: Time-resolved particle image velocimetry investigation
Zhang et al. Experimental study of plasma flow control on highly swept delta wing
Sidorenko et al. Suppression of transonic buffet with plasma vortex generators
Sekimoto et al. Experimental Study of Effects of Frequency for Burst Wave on a DBD Plasma Actuator for Separation
Esfahani et al. Flow separation control over a Boeing Vertol VR-7 using NS-DBD plasma actuators
Asada et al. Computational analysis of unsteady flow-field induced by plasma actuator in burst mode
Güler et al. Effect of signal modulation of DBD plasma actuator on flow control around NACA 0015
Pierre et al. Unsteady forcing of a post-stall flow over N NACA0012 airfoil by A surface DBD actuator
Sato et al. Effective mechanisms for turbulent-separation control by DBD plasma actuator around NACA0015 at reynolds number 1,600,000
Cui et al. Separation control over a NACA0015 airfoil using nanosecond pulsed plasma actuator
Chen et al. Shock-induced separation control by using nanosecond pulsed SDBD plasma actuators
DeSalvo et al. Enhancement of a high-lift airfoil using low-power fluidic actuators
Farnsworth et al. Aerodynamic performance modification of the stingray UAV at low angles of attack
Wong et al. A high-performing sawtooth plasma actuator with multi-electrodes
Sekimoto et al. Experimental study of burst ratio effect for dielectric-barrier-discharge plasma actuator for separation control
Vishnyakov et al. Control of buffet onset by plasma-based actuators
Sidorenko et al. Transonic buffet control by plasma actuator with spark discharge
Post et al. Effects of an Aerodynamic Plasma Actuator on a HSNLF Airfoil
Veldhuis et al. Novel passive and active flow control for high lift
Erfani et al. MEE-DBD plasma actuator effect on aerodynamics of a NACA0015 aerofoil: Separation and 3D wake
Sekimoto et al. Experimental study of a nano-second pulse plasma actuator for low reynolds number flow control