DE1456056A1 - Tragflaeche mit Auftriebswirkung fuer Flugzeuge - Google Patents

Tragflaeche mit Auftriebswirkung fuer Flugzeuge

Info

Publication number
DE1456056A1
DE1456056A1 DE19651456056 DE1456056A DE1456056A1 DE 1456056 A1 DE1456056 A1 DE 1456056A1 DE 19651456056 DE19651456056 DE 19651456056 DE 1456056 A DE1456056 A DE 1456056A DE 1456056 A1 DE1456056 A1 DE 1456056A1
Authority
DE
Germany
Prior art keywords
wing
aircraft
lift effect
lift
effect
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.)
Pending
Application number
DE19651456056
Other languages
English (en)
Inventor
Lemoigne Pierre Marcel
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.)
LEMOIGNE PIERRE MARCEL
Original Assignee
LEMOIGNE PIERRE MARCEL
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 LEMOIGNE PIERRE MARCEL filed Critical LEMOIGNE PIERRE MARCEL
Publication of DE1456056A1 publication Critical patent/DE1456056A1/de
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
    • B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
    • 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
    • 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
    • B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
    • 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
    • B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • 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
    • B64C2230/20—Boundary layer controls by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Description

  • Tragfläche mit Auftriebawirkung für Flugseuge
DE19651456056 1964-11-23 1965-10-12 Tragflaeche mit Auftriebswirkung fuer Flugzeuge Pending DE1456056A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR995922A FR1423830A (fr) 1964-11-23 1964-11-23 Surface portante hypersustentatrice pour aéronefs

Publications (1)

Publication Number Publication Date
DE1456056A1 true DE1456056A1 (de) 1970-01-22

Family

ID=8843106

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19651456056 Pending DE1456056A1 (de) 1964-11-23 1965-10-12 Tragflaeche mit Auftriebswirkung fuer Flugzeuge

Country Status (5)

Country Link
US (1) US3366348A (de)
BE (1) BE671479A (de)
DE (1) DE1456056A1 (de)
FR (1) FR1423830A (de)
GB (1) GB1119419A (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3884172A (en) * 1974-01-02 1975-05-20 Kenryu Takahashi Hydroplane boat
ATE33806T1 (de) * 1982-08-03 1988-05-15 Horst Dr Med Kief Gleitfluggeraet mit variabler gleitzahl.
US6138957A (en) * 1998-12-23 2000-10-31 Northrop Grumman Corporation Swept-back wings with airflow channeling
US7357351B2 (en) * 2002-07-18 2008-04-15 Eric T. Schmidt Linear shock wave absorber
US8113469B2 (en) * 2006-02-21 2012-02-14 University Of Alabama Passive micro-roughness array for drag modification
US8794574B2 (en) * 2007-03-30 2014-08-05 The Board Of Trustees Of The University Of Alabama Micro-array surface for passive drag modification
GB201114433D0 (en) * 2011-08-22 2011-10-05 Airbus Operations Ltd Wing leading edge venting

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3281095A (en) * 1964-06-11 1966-10-25 Thomas M Runge Aircraft wing and means to reduce stalling tendency of wing and to facilitate recovery from stalling
US3269674A (en) * 1964-06-26 1966-08-30 Ryan Aeronautical Co Flexible wing with pitch stabilizing means

Also Published As

Publication number Publication date
GB1119419A (en) 1968-07-10
BE671479A (de) 1966-02-14
US3366348A (en) 1968-01-30
FR1423830A (fr) 1966-01-07

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