SE7414920L - - Google Patents
Info
- Publication number
- SE7414920L SE7414920L SE7414920A SE7414920A SE7414920L SE 7414920 L SE7414920 L SE 7414920L SE 7414920 A SE7414920 A SE 7414920A SE 7414920 A SE7414920 A SE 7414920A SE 7414920 L SE7414920 L SE 7414920L
- Authority
- SE
- Sweden
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19732361888 DE2361888C3 (de) | 1973-12-13 | Steuer- und Stabilisierungseinrichtung für ein Flugzeug künstlicher Stabilität |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SE7414920L true SE7414920L (ja) | 1975-06-16 |
Family
ID=5900576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE7414920A SE7414920L (ja) | 1973-12-13 | 1974-11-28 |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR2254481A1 (ja) |
| SE (1) | SE7414920L (ja) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1152763B (it) * | 1982-01-25 | 1987-01-14 | Ind Aeronautiche E Meccaniche | Aeromobile perfezionato |
| US4723214A (en) * | 1985-02-15 | 1988-02-02 | Grumman Aerospace Corporation | Automatic camber control |
| CN109598025B (zh) * | 2018-11-02 | 2023-05-26 | 中国航空工业集团公司西安飞机设计研究所 | 一种v形尾翼倾角与面积优化设计方法 |
| CN110395389A (zh) * | 2019-06-28 | 2019-11-01 | 中国航天空气动力技术研究院 | 一种改善高超声速飞行器横侧向耦合特性的气动布局 |
-
1974
- 1974-11-28 SE SE7414920A patent/SE7414920L/xx unknown
- 1974-12-11 FR FR7440848A patent/FR2254481A1/fr not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| FR2254481A1 (en) | 1975-07-11 |
| DE2361888A1 (de) | 1975-06-19 |
| DE2361888B2 (de) | 1976-06-10 |