FR2401061A1 - Fuselage aerodynamique - Google Patents

Fuselage aerodynamique

Info

Publication number
FR2401061A1
FR2401061A1 FR7726075A FR7726075A FR2401061A1 FR 2401061 A1 FR2401061 A1 FR 2401061A1 FR 7726075 A FR7726075 A FR 7726075A FR 7726075 A FR7726075 A FR 7726075A FR 2401061 A1 FR2401061 A1 FR 2401061A1
Authority
FR
France
Prior art keywords
delta
stationary
engine intake
aerofoil profile
drawn over
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
FR7726075A
Other languages
English (en)
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
Priority to FR7726075A priority Critical patent/FR2401061A1/fr
Publication of FR2401061A1 publication Critical patent/FR2401061A1/fr
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/0009Aerodynamic aspects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045Fuselages characterised by special shapes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Fuselage aérodynamique ayant une forme en plan à symétrie bilatérale, comprenant une section avant, une section arrière et deux panneaux latéraux, caractérisé en ce que la section avant est de forme en plan à peu près triangulaire et présente un profil d'aile en vue de côte, la section arrière présente un profil d'aile en vue de côté, et les panneaux latéraux s'étendent transversalement par rapport à l'axe de fuselage dans des directions opposées à partir de la section arrière, chacun de ces panneaux latéraux étant de longueur progressivement croissante, dans la direction transversale à l'axe du fuselage, depuis sa partie la plus antérieure en direction de l'arrière jusqu'au moins la moitié de la distance allant jusqu'à sa partie située le plus à l'arrière, chaque panneau latéral ayant un profil d'aile en vue de côté.
FR7726075A 1977-08-26 1977-08-26 Fuselage aerodynamique Pending FR2401061A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7726075A FR2401061A1 (fr) 1977-08-26 1977-08-26 Fuselage aerodynamique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7726075A FR2401061A1 (fr) 1977-08-26 1977-08-26 Fuselage aerodynamique

Publications (1)

Publication Number Publication Date
FR2401061A1 true FR2401061A1 (fr) 1979-03-23

Family

ID=9194809

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7726075A Pending FR2401061A1 (fr) 1977-08-26 1977-08-26 Fuselage aerodynamique

Country Status (1)

Country Link
FR (1) FR2401061A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2457803A1 (fr) * 1979-05-31 1980-12-26 Marcillaud Jean Pierre Aile et coque de patin hydroglisseur ou d'avion permettant une grande stabilite en vol supersonique et subsonique avec des ailes de grandes surfaces et de faible epaisseur

Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2039179A (en) * 1933-07-05 1936-04-28 Mazxini Franco Air-circulation valve in the supporting surfaces of aeroplanes
GB510546A (en) * 1938-02-07 1939-08-03 Alfred Richard Weyl Improvements relating to high-lift aerofoils
DE735881C (de) * 1940-07-05 1943-05-31 Messerschmitt A G Quersteuereinrichtung fuer Flugzeuge mit an den Tragfluegeln angelenkten Stoerklappen
FR964101A (fr) * 1950-08-07
FR984966A (fr) * 1943-10-20 1951-07-12 Surface aérodynamique à fente suralimentée et aérodynes en comportant application
US2586299A (en) * 1945-09-11 1952-02-19 Vincent J Burnelli Airplane provided with jet propulsion means
US2696953A (en) * 1951-03-09 1954-12-14 Collins Radio Co Fluid propelled airplane
GB783087A (en) * 1953-01-20 1957-09-18 Francis James Eckington Aircraft
US2987277A (en) * 1958-10-14 1961-06-06 North American Aviation Inc Aircraft control system
US3097817A (en) * 1962-04-05 1963-07-16 Jr Hugh E Towzey Airfoil design for jet engined aircraft
GB1028602A (en) * 1963-04-30 1966-05-04 British Aircraft Corp Ltd Improvements in and relating to hypersonic speed aircraft
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
US3430446A (en) * 1964-04-20 1969-03-04 Us Navy External burning ramjet engine
US3478989A (en) * 1966-11-14 1969-11-18 Hamburger Flugzeugbau Gmbh Supersonic aircraft
US3576300A (en) * 1968-08-01 1971-04-27 Rolls Royce Aircraft
US3684217A (en) * 1970-09-30 1972-08-15 Aereon Corp Aircraft

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR964101A (fr) * 1950-08-07
US2039179A (en) * 1933-07-05 1936-04-28 Mazxini Franco Air-circulation valve in the supporting surfaces of aeroplanes
GB510546A (en) * 1938-02-07 1939-08-03 Alfred Richard Weyl Improvements relating to high-lift aerofoils
DE735881C (de) * 1940-07-05 1943-05-31 Messerschmitt A G Quersteuereinrichtung fuer Flugzeuge mit an den Tragfluegeln angelenkten Stoerklappen
FR984966A (fr) * 1943-10-20 1951-07-12 Surface aérodynamique à fente suralimentée et aérodynes en comportant application
US2586299A (en) * 1945-09-11 1952-02-19 Vincent J Burnelli Airplane provided with jet propulsion means
US2696953A (en) * 1951-03-09 1954-12-14 Collins Radio Co Fluid propelled airplane
GB783087A (en) * 1953-01-20 1957-09-18 Francis James Eckington Aircraft
US2987277A (en) * 1958-10-14 1961-06-06 North American Aviation Inc Aircraft control system
US3097817A (en) * 1962-04-05 1963-07-16 Jr Hugh E Towzey Airfoil design for jet engined aircraft
GB1028602A (en) * 1963-04-30 1966-05-04 British Aircraft Corp Ltd Improvements in and relating to hypersonic speed aircraft
US3430446A (en) * 1964-04-20 1969-03-04 Us Navy External burning ramjet engine
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
US3478989A (en) * 1966-11-14 1969-11-18 Hamburger Flugzeugbau Gmbh Supersonic aircraft
US3576300A (en) * 1968-08-01 1971-04-27 Rolls Royce Aircraft
US3684217A (en) * 1970-09-30 1972-08-15 Aereon Corp Aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2457803A1 (fr) * 1979-05-31 1980-12-26 Marcillaud Jean Pierre Aile et coque de patin hydroglisseur ou d'avion permettant une grande stabilite en vol supersonique et subsonique avec des ailes de grandes surfaces et de faible epaisseur

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