FR2272893A1 - Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators - Google Patents
Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevatorsInfo
- Publication number
- FR2272893A1 FR2272893A1 FR7508295A FR7508295A FR2272893A1 FR 2272893 A1 FR2272893 A1 FR 2272893A1 FR 7508295 A FR7508295 A FR 7508295A FR 7508295 A FR7508295 A FR 7508295A FR 2272893 A1 FR2272893 A1 FR 2272893A1
- Authority
- FR
- France
- Prior art keywords
- front wing
- small
- elevators
- aircraft
- wings
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/04—Noseplanes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1193274 | 1974-03-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2272893A1 true FR2272893A1 (en) | 1975-12-26 |
FR2272893B3 FR2272893B3 (de) | 1977-11-25 |
Family
ID=9995305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7508295A Granted FR2272893A1 (en) | 1974-03-18 | 1975-03-17 | Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2272893A1 (de) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4116405A (en) * | 1977-03-28 | 1978-09-26 | Grumman Aerospace Corporation | Airplane |
FR2473466A1 (fr) * | 1980-01-09 | 1981-07-17 | Airbus Ind | Avion a voilure fixe comportant des surfaces portantes placees en tandem |
-
1975
- 1975-03-17 FR FR7508295A patent/FR2272893A1/fr active Granted
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4116405A (en) * | 1977-03-28 | 1978-09-26 | Grumman Aerospace Corporation | Airplane |
FR2473466A1 (fr) * | 1980-01-09 | 1981-07-17 | Airbus Ind | Avion a voilure fixe comportant des surfaces portantes placees en tandem |
EP0033053B1 (de) * | 1980-01-09 | 1984-07-18 | Airbus Industrie | Flugzeug mit festen Flügeln, bei denen die Tragflächen in Tandemform angeordnet sind |
Also Published As
Publication number | Publication date |
---|---|
FR2272893B3 (de) | 1977-11-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1427802A (en) | Aircraft | |
Parlett | Wind-Tunnel Investigation of an External-Flow Jet-Flap Transport Configuration Having Full-Span Triple-Slotted Flaps | |
US3795373A (en) | Aircraft | |
US2628043A (en) | Tailless airplane | |
FR2272893A1 (en) | Powered aircraft with small front wing - has freely rotating tabs on front wing forming elevators | |
GB1103974A (en) | Pitch-stabilized airplane wing | |
GB1112924A (en) | Improvements in or relating to aircraft | |
BOWMAN, JR et al. | Correlation of model and airplane spin characteristics for a low-wing general aviation research airplane | |
Foster et al. | Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-Sweep Wings | |
FR2309401A1 (fr) | Rotor sustentateur propulsif | |
GB987792A (en) | Improvements in and relating to aircraft wings | |
GB593032A (en) | Improvements in or relating to aircraft | |
Foster et al. | Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a Variable-Wing-Sweep STOL Configuration | |
GB432245A (en) | Improvements in aircraft of the helicopter type | |
Day et al. | Flight Behavior of the X-2 Research Airplane to a Mach Number of 3.20 and a Geometric Altitude of 126,200 Feet | |
GB1169880A (en) | Aircraft having Means to Counteract Displacement of the Aerodynamic Centre | |
GB448703A (en) | Improvements in or relating to aircraft fuselages | |
Červinka et al. | AN AIRPLANE WITH UNCONVENTIONALLY PLACED PROPELLER POWER UNIT | |
Morris et al. | A Limited Investigation of the Effect of Three Vortex-generator Configuration on the Effectiveness of a Plain Flap on an Unswept Wing | |
WING et al. | NATIONAL ADVISORY COMMITTEE FOR AERONA UTIes | |
DICARLO et al. | Exploratory study of the influence of wing leading-edge modifications on the spin characteristics of a low-wing single-engine general aviation airplane | |
ROSENSTEIN et al. | Cyclic pitch control on a V/STOL tilt-wing aircraft(Performance of cyclic pitch propellers for longitudinal control of V/STOL tilt wing aircraft) | |
GB563467A (en) | Improvements in aircraft | |
GB718435A (en) | Improvements in aeroplane control organs | |
SALTERS | Longitudinal aerodynamic and propulsion characteristics of a propulsive-wing V/STOL model at high subsonic speeds(Wind tunnel tests to determine aerodynamic and propulsion characteristics of propulsive wing V/STOL configuration at high subsonic speed) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |