Little et al., 2010 - Google Patents
High-lift airfoil separation with dielectric barrier discharge plasma actuationLittle et al., 2010
- Document ID
- 17990178790946487403
- Author
- Little J
- Samimy M
- Publication year
- Publication venue
- AIAA journal
External Links
Snippet
HIGH-LIFT airfoils typically employ trailing-edge (TE) flaps that can be deflected during takeoff or landing and stowed during cruise. Such devices enhance the lift of conventional airfoils, but can impose a penalty, due to flow separation that occurs when the momentum of …
- 238000000926 separation method 0 title abstract description 64
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
- Y02T50/60—Efficient propulsion technologies
- Y02T50/67—Relevant aircraft propulsion technologies
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/17—Purpose of the control system to control boundary layer
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Little et al. | High-lift airfoil separation with dielectric barrier discharge plasma actuation | |
| Huang et al. | Unsteady plasma actuators for separation control of low-pressure turbine blades | |
| Little et al. | High-lift airfoil trailing edge separation control using a single dielectric barrier discharge plasma actuator | |
| Volino | Separation control on low-pressure turbine airfoils using synthetic vortex generator jets | |
| Goeksel et al. | Steady and unsteady plasma wall jets for separation and circulation control | |
| Moreau et al. | Control of a turbulent flow separated at mid-chord along an airfoil with DBD plasma actuators | |
| Rethmel et al. | Flow separation control using nanosecond pulse driven DBD plasma actuators. | |
| US20080067283A1 (en) | Methods and apparatus for reducing noise via a plasma fairing | |
| Downs III et al. | Free-stream turbulence and the development of cross-flow disturbances | |
| Melton et al. | Active control of separation from the flap of a supercritical airfoil | |
| Little et al. | High lift airfoil leading edge separation control with nanosecond pulse DBD plasma actuators | |
| Zhang et al. | Turbulent boundary layer separation control using plasma actuator at Reynolds number 2000000 | |
| Greenblatt et al. | Delta-wing flow control using dielectric barrier discharge actuators | |
| Mirzaei et al. | Experimental study of vortex shedding control using plasma actuator | |
| Ruisi et al. | Active flow control over a backward-facing step using plasma actuation | |
| Ebrahimi et al. | Experimental study of stall control over an airfoil with dual excitation of separated shear layers | |
| Post et al. | Flow control with single dielectric barrier plasma actuators | |
| Mabe et al. | Single dielectric barrier discharge plasma actuators for improved airfoil performance | |
| Esfahani et al. | Flow separation control over a Boeing Vertol VR-7 using NS-DBD plasma actuators | |
| Ben Chiekh et al. | Aerodynamic flow vectoring of a wake using asymmetric synthetic jet actuation | |
| Güler et al. | Effect of signal modulation of DBD plasma actuator on flow control around NACA 0015 | |
| Huang et al. | Plasma actuators for noise control | |
| KV et al. | Advancements in flow control using plasma actuators: a comprehensive review | |
| Pack Melton et al. | Application of excitation from multiple locations on a simplified high-lift system | |
| Boesch et al. | Flight control using wing-tip plasma actuation |