FR2401061A1 - Fuselage aerodynamique - Google Patents
Fuselage aerodynamiqueInfo
- 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
Links
- 241000272517 Anseriformes Species 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/0009—Aerodynamic aspects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0045—Fuselages 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.
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)
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)
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 |
-
1977
- 1977-08-26 FR FR7726075A patent/FR2401061A1/fr active Pending
Patent Citations (16)
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)
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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