FR1241405A - Aerodynamic wing profile plan - Google Patents
Aerodynamic wing profile planInfo
- Publication number
- FR1241405A FR1241405A FR810426A FR810426A FR1241405A FR 1241405 A FR1241405 A FR 1241405A FR 810426 A FR810426 A FR 810426A FR 810426 A FR810426 A FR 810426A FR 1241405 A FR1241405 A FR 1241405A
- Authority
- FR
- France
- Prior art keywords
- wing profile
- aerodynamic wing
- profile plan
- plan
- aerodynamic
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1241405XA | 1958-12-15 | 1958-12-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1241405A true FR1241405A (en) | 1960-09-16 |
Family
ID=22413014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR810426A Expired FR1241405A (en) | 1958-12-15 | 1959-11-17 | Aerodynamic wing profile plan |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1241405A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4099691A (en) * | 1976-12-13 | 1978-07-11 | The Boeing Company | Boundary layer control system for aircraft |
US5114102A (en) * | 1989-10-06 | 1992-05-19 | The Boeing Company | Boundary layer control |
-
1959
- 1959-11-17 FR FR810426A patent/FR1241405A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4099691A (en) * | 1976-12-13 | 1978-07-11 | The Boeing Company | Boundary layer control system for aircraft |
US5114102A (en) * | 1989-10-06 | 1992-05-19 | The Boeing Company | Boundary layer control |
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