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

Balcer et al., 2006 - Google Patents

Effects of plasma induced velocity on boundary layer flow

Balcer et al., 2006

Document ID
9935507319471610924
Author
Balcer B
Franke M
Rivir R
Publication year
Publication venue
44th AIAA Aerospace Sciences Meeting and Exhibit

External Links

Snippet

The use of a plasma to control boundary layers has been studied in low speed wind tunnels for a number of years. In 1998, researchers at the University of Tennessee created a blue print for the types of electrodes that work best when dealing with plasmas at atmospheric …
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
Huang et al. Unsteady plasma actuators for separation control of low-pressure turbine blades
Little et al. High-lift airfoil separation with dielectric barrier discharge plasma actuation
Santhanakrishnan et al. Flow control using plasma actuators and linear/annular plasma synthetic jet actuators
Al-Sadawi et al. Aerodynamic noise reduction by plasma actuators for a flat plate with blunt trailing edge
Sidorenko et al. Plasma control of vortex flow on a delta wing at high angles of attack
Giuni Formation and early development of wingtip vortices
Little et al. High lift airfoil leading edge separation control with nanosecond pulse DBD plasma actuators
Porter et al. Spatially distributed forcing and jet vectoring with a plasma actuator
Schatzman et al. Turbulent boundary-layer separation control with single dielectric barrier discharge plasma actuators
Evans et al. Separation-control mechanisms of steady and pulsed vortex-generator jets
Balcer et al. Effects of plasma induced velocity on boundary layer flow
Esfahani et al. Flow separation control over a thin post-stall airfoil: effects of excitation frequency
Ramakumar Flow control and lift enhancement using plasma actuators
Güler et al. Effect of signal modulation of DBD plasma actuator on flow control around NACA 0015
Bolitho et al. Thrust vectoring flow control using plasma synthetic jet actuators
Ashcraft et al. Control of boundary layer separation and the wake of an airfoil using ns-DBD plasma actuators
Raghunathan Pressure fluctuation measurements with passive shock/boundary-layer control
Wong et al. A high-performing sawtooth plasma actuator with multi-electrodes
Huang et al. Turbulent flows of an acoustically excited elevated transverse jet
Abbasi et al. Thermal characteristics of plasma actuators in turbulent boundary layer
Santhanakrishnan et al. Effect of plasma morphology on flow control using plasma synthetic jet actuators
Kontis et al. Flow control at subsonic speeds using serpentine plasma actuators
Fletcher et al. Characterization of Periodic Unsteadiness Generator for Secondary Flow Studies
Zare-Behtash et al. Flow control at subsonic speeds using serpentine plasma actuators
Ghassemi Isfahani et al. Stall cell formation over a Boeing Vertol VR-7 airfoil