[go: up one dir, main page]

Anderson et al. - Google Patents

i, United States Patent (10) Patent No.: US 8.382. 029 B2

Anderson et al.

View PDF
Document ID
7526610941854359935
Author
Anderson R
et al.

External Links

Snippet

3,150,483 A* 9/1964 Mayfield et al........................... 6 ()/2 () 2 3,177.654 A* 4/1965 Gradecak 244/23 R 5,669.583 A 9/1997 Ryth 5938854 A 8/1999 Ryth 6.200. 539 B1* 3/2001 Sherman et al....................... 2 16/67 6.247. 671 B1 6/2001 Saeks et al. of airfoil efficiency due to the …
Continue reading at faculty.eng.ufl.edu (PDF) (other versions)

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2230/00Boundary layer controls
    • B64C2230/12Boundary layer controls by using electromagnetic tiles, fluid ionizers, static charges or plasma
    • 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies

Similar Documents

Publication Publication Date Title
US8960595B2 (en) Wingless hovering of micro air vehicle
US8708651B2 (en) Aerodynamic performance enhancements using discharge plasma actuators
US20230202646A1 (en) Method and apparatus for mitigating trailing vortex wakes of lifting or thrust generating bodies
US8235072B2 (en) Method and apparatus for multibarrier plasma actuated high performance flow control
AU2014262214B2 (en) Plasma-assisted synthetic jets for active air flow control
EP1926353A1 (en) Over-wing travelling-wave axial flow plasma accelerator
US5320309A (en) Electromagnetic device and method for boundary layer control
Liu et al. Aerodynamic control of NACA 0021 airfoil model with spark discharge plasma synthetic jets
Anderson i, United States Patent (10) Patent No.: US 8.382. 029 B2
HK1129642B (en) Wingless hovering of micro air vehicle
Leng et al. Electrohydrodynamic thrust with no combustion emissions and noises in a centimeter-scale point-to-grid configuration
Mai et al. Development of boat model powered by electro-hydrodynamic propulsion system
Blondeau et al. Wind tunnel testing of a morphing aspect ratio wing using an pneumatic telescoping spar
Petit et al. MHD hypersonic flow control for aerospace applications
CN119329747B (en) Turbulent friction drag reduction device and method based on array corona discharge
Nishida et al. Preliminary experimental study on aerodynamic characteristics control of slender body using DBD plasma actuator
Nadar et al. Plasma Blade Propulsion: Unmanned Aerial Vehicles
Bolitho et al. Active vortex generators using jet vectoring plasma actuators
Ying et al. Simple Electroaerodynamic Aircraft Testing with Multistage Staggered Arrangement of the Electrodes
Madhan et al. Aerodynamic flow control by peristaltic acceleration of a one atmosphere uniform glow discharge plasma
Dahm et al. Microactuator array for sublayer control in turbulent boundary layers using the electrokinetic principles
Marqués Aerodynamics of the UCAV 1303 delta-wing configuration and flow structure modification using plasma actuators