RU94033526A - Aircraft wing tip - Google Patents
Aircraft wing tipInfo
- Publication number
- RU94033526A RU94033526A RU94033526/11A RU94033526A RU94033526A RU 94033526 A RU94033526 A RU 94033526A RU 94033526/11 A RU94033526/11 A RU 94033526/11A RU 94033526 A RU94033526 A RU 94033526A RU 94033526 A RU94033526 A RU 94033526A
- Authority
- RU
- Russia
- Prior art keywords
- wing
- aircraft
- ledge
- profiles
- line
- Prior art date
Links
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Tires In General (AREA)
Abstract
FIELD: aeronautical engineering; aeroplanes of various purpose. SUBSTANCE: wing tip has step made in plane of wing in its nose portion; profiles of step have increased curvature and increased angle of warping. Wing leading edge is provided with sharp end edge before step smoothly changing to blunt leading edge and line of maximum thicknesses of step profiles is shifted at top backward relative to similar line of wing and is located within 60 to 80 percent of local wing chord. EFFECT: improved aerodynamic property of aircraft at subsonic and transonic speeds of flight. 2 cl, 6 dwg
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU94033526A RU2086467C1 (en) | 1994-09-15 | 1994-09-15 | Aircraft wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU94033526A RU2086467C1 (en) | 1994-09-15 | 1994-09-15 | Aircraft wing |
Publications (2)
Publication Number | Publication Date |
---|---|
RU94033526A true RU94033526A (en) | 1996-07-10 |
RU2086467C1 RU2086467C1 (en) | 1997-08-10 |
Family
ID=20160458
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU94033526A RU2086467C1 (en) | 1994-09-15 | 1994-09-15 | Aircraft wing |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2086467C1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009019542A1 (en) | 2009-04-30 | 2010-11-11 | Airbus Deutschland Gmbh | Non-planar wing tail for airplanes of aircraft and wings with such wing tail |
RU2495787C1 (en) * | 2012-04-26 | 2013-10-20 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Aircraft wing tip |
-
1994
- 1994-09-15 RU RU94033526A patent/RU2086467C1/en active
Also Published As
Publication number | Publication date |
---|---|
RU2086467C1 (en) | 1997-08-10 |
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