AU4214789A - Generation of an aerodynamic force by lateral blowing of air at the underwing of aircraft wings from the wing extremities towards the wing root at the aircraft fuselage - Google Patents

Generation of an aerodynamic force by lateral blowing of air at the underwing of aircraft wings from the wing extremities towards the wing root at the aircraft fuselage

Info

Publication number
AU4214789A
AU4214789A AU42147/89A AU4214789A AU4214789A AU 4214789 A AU4214789 A AU 4214789A AU 42147/89 A AU42147/89 A AU 42147/89A AU 4214789 A AU4214789 A AU 4214789A AU 4214789 A AU4214789 A AU 4214789A
Authority
AU
Australia
Prior art keywords
wing
aircraft
underwing
generation
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU42147/89A
Inventor
Bernard Edouard Emilien Touret
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of AU4214789A publication Critical patent/AU4214789A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU42147/89A 1988-08-30 1989-08-25 Generation of an aerodynamic force by lateral blowing of air at the underwing of aircraft wings from the wing extremities towards the wing root at the aircraft fuselage Abandoned AU4214789A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8811352A FR2635750A1 (en) 1988-08-30 1988-08-30 CREATION OF AERODYNAMIC FORCE BY LATERAL AIR BLOWING INTO THE INTRADOS OF AN AIRCRAFT VESSEL, FROM ITS EXTREMITES TO ITS EMPLANTURE IN FUSELAGE OF THE AIRPLANE
FR8811352 1988-08-30

Publications (1)

Publication Number Publication Date
AU4214789A true AU4214789A (en) 1990-03-23

Family

ID=9369592

Family Applications (1)

Application Number Title Priority Date Filing Date
AU42147/89A Abandoned AU4214789A (en) 1988-08-30 1989-08-25 Generation of an aerodynamic force by lateral blowing of air at the underwing of aircraft wings from the wing extremities towards the wing root at the aircraft fuselage

Country Status (3)

Country Link
AU (1) AU4214789A (en)
FR (1) FR2635750A1 (en)
WO (1) WO1990002079A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19734770A1 (en) * 1997-08-11 1999-02-18 Tina Artinger Fluid dynamic profile

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR850918A (en) * 1938-09-05 1939-12-29 Improvements to air navigation devices
US3480234A (en) * 1967-08-18 1969-11-25 Lockheed Aircraft Corp Method and apparatus for modifying airfoil fluid flow

Also Published As

Publication number Publication date
FR2635750A1 (en) 1990-03-02
WO1990002079A1 (en) 1990-03-08

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