FR654236A - - Google Patents
Info
- Publication number
- FR654236A FR654236A FR654236DA FR654236A FR 654236 A FR654236 A FR 654236A FR 654236D A FR654236D A FR 654236DA FR 654236 A FR654236 A FR 654236A
- Authority
- FR
- France
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
- B64C3/50—Varying camber by leading or trailing edge flaps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
FR654236A true FR654236A (en) | 1929-04-03 |
Family
ID=1543019
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR654236D Expired FR654236A (en) |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR654236A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3003239B1 (en) * | 1980-01-30 | 1981-05-14 | Hermann Dr. 8510 Fürth Neuhierl | Airfoil with adjustable profile for a model airplane |
DE3816431A1 (en) * | 1988-05-13 | 1989-11-16 | Otilio Nemec | Intermediate-stage curvature device for aerodynamic control surfaces |
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0
- FR FR654236D patent/FR654236A/fr not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3003239B1 (en) * | 1980-01-30 | 1981-05-14 | Hermann Dr. 8510 Fürth Neuhierl | Airfoil with adjustable profile for a model airplane |
DE3816431A1 (en) * | 1988-05-13 | 1989-11-16 | Otilio Nemec | Intermediate-stage curvature device for aerodynamic control surfaces |