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FR1522282A - Method and device for improving the yaw stability of aerodynes at high incidence of flight - Google Patents

Method and device for improving the yaw stability of aerodynes at high incidence of flight

Info

Publication number
FR1522282A
FR1522282A FR95036A FR95036A FR1522282A FR 1522282 A FR1522282 A FR 1522282A FR 95036 A FR95036 A FR 95036A FR 95036 A FR95036 A FR 95036A FR 1522282 A FR1522282 A FR 1522282A
Authority
FR
France
Prior art keywords
aerodynes
flight
improving
high incidence
yaw stability
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.)
Expired
Application number
FR95036A
Other languages
French (fr)
Inventor
Georges Sabathe
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.)
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Original Assignee
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
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 Sud Aviation Societe Nationale de Constructions Aerdnaettiques filed Critical Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Priority to FR95036A priority Critical patent/FR1522282A/en
Application granted granted Critical
Publication of FR1522282A publication Critical patent/FR1522282A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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)
FR95036A 1967-02-15 1967-02-15 Method and device for improving the yaw stability of aerodynes at high incidence of flight Expired FR1522282A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR95036A FR1522282A (en) 1967-02-15 1967-02-15 Method and device for improving the yaw stability of aerodynes at high incidence of flight

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR95036A FR1522282A (en) 1967-02-15 1967-02-15 Method and device for improving the yaw stability of aerodynes at high incidence of flight

Publications (1)

Publication Number Publication Date
FR1522282A true FR1522282A (en) 1968-04-26

Family

ID=8625326

Family Applications (1)

Application Number Title Priority Date Filing Date
FR95036A Expired FR1522282A (en) 1967-02-15 1967-02-15 Method and device for improving the yaw stability of aerodynes at high incidence of flight

Country Status (1)

Country Link
FR (1) FR1522282A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2480704A1 (en) * 1980-04-18 1981-10-23 Secr Defence Brit IMPROVEMENTS ON COMBAT AIRCRAFT WITH LATERAL STABILIZATION DEVICES
EP0052360A1 (en) * 1980-11-15 1982-05-26 Fuji Jukogyo Kabushiki Kaisha Air aspiration device of aircraft-mounted gas-turbine engine
EP0188826A2 (en) * 1984-12-31 1986-07-30 The Boeing Company Improved vortex generator
US5150858A (en) * 1989-03-11 1992-09-29 British Aerospace Public Limited Company Jettisonable aerodynamic control surfaces
US5366180A (en) * 1993-06-30 1994-11-22 Northrop Corporation High-lift device for aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2480704A1 (en) * 1980-04-18 1981-10-23 Secr Defence Brit IMPROVEMENTS ON COMBAT AIRCRAFT WITH LATERAL STABILIZATION DEVICES
US4378922A (en) * 1980-04-18 1983-04-05 The Secretary Of State For Defence In Her Brittannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Aircraft having improved strake configuration
EP0052360A1 (en) * 1980-11-15 1982-05-26 Fuji Jukogyo Kabushiki Kaisha Air aspiration device of aircraft-mounted gas-turbine engine
EP0188826A2 (en) * 1984-12-31 1986-07-30 The Boeing Company Improved vortex generator
EP0188826A3 (en) * 1984-12-31 1986-08-13 The Boeing Company Improved vortex generator
US5150858A (en) * 1989-03-11 1992-09-29 British Aerospace Public Limited Company Jettisonable aerodynamic control surfaces
US5366180A (en) * 1993-06-30 1994-11-22 Northrop Corporation High-lift device for aircraft

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