FR912435A - Method and device for the high lift of aerodynes - Google Patents
Method and device for the high lift of aerodynesInfo
- Publication number
- FR912435A FR912435A FR912435DA FR912435A FR 912435 A FR912435 A FR 912435A FR 912435D A FR912435D A FR 912435DA FR 912435 A FR912435 A FR 912435A
- Authority
- FR
- France
- Prior art keywords
- aerodynes
- high lift
- lift
- 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
Links
Classifications
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR912435T | 1945-02-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR912435A true FR912435A (en) | 1946-08-08 |
Family
ID=9421322
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR912435D Expired FR912435A (en) | 1945-02-27 | 1945-02-27 | Method and device for the high lift of aerodynes |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR912435A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1147850B (en) * | 1956-05-31 | 1963-04-25 | United Aircraft Corp | Aircraft wing with low aspect ratio |
FR2485654A1 (en) * | 1980-06-24 | 1981-12-31 | Nazare Edgard | Generator to reduce fluid resistance of vehicles moving in it - uses angled jets to give aerodynamic flow over vehicle |
ES2289920A1 (en) * | 2006-03-14 | 2008-02-01 | Juan Carlos Santalo Barrios | Dynamic flow counterattack system is designed for vehicle, which move in fluids, where system is based on generation of air currents, which is perpendicular to advance direction, generating turbulent current zone of small pressure |
-
1945
- 1945-02-27 FR FR912435D patent/FR912435A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1147850B (en) * | 1956-05-31 | 1963-04-25 | United Aircraft Corp | Aircraft wing with low aspect ratio |
FR2485654A1 (en) * | 1980-06-24 | 1981-12-31 | Nazare Edgard | Generator to reduce fluid resistance of vehicles moving in it - uses angled jets to give aerodynamic flow over vehicle |
ES2289920A1 (en) * | 2006-03-14 | 2008-02-01 | Juan Carlos Santalo Barrios | Dynamic flow counterattack system is designed for vehicle, which move in fluids, where system is based on generation of air currents, which is perpendicular to advance direction, generating turbulent current zone of small pressure |
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