FIELD: aeronautical engineering. SUBSTANCE: wing has tip mounted in its plane and provided with shoulder over leading edge; tip has profiles of increased camber as compared with wing and twist angles; end edge of tip before shoulder is sharp smoothly changing into blunt leading edge after shoulder; line of maximum thickness of above-chord section of tip profiles is shifted backward after shoulder over upper contour and is located within 60-80% of local chord of tip. EFFECT: enhanced efficiency. 2 cl, 5 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| AIRCRAFT WING TIP | 2000 | 
 | RU2173655C1 | 
| AIRCRAFT WING TIP | 2012 | 
 | RU2495787C1 | 
| TIP OF FLYING VEHICLE LIFTING SURFACE | 2001 | 
 | RU2216480C2 | 
| AIRCRAFT WING TIP | 2008 | 
 | RU2378154C1 | 
| AIRCRAFT WINGTIP | 2016 | 
 | RU2637233C1 | 
| FLYING VEHICLE LIFTING SURFACE TIP | 2004 | 
 | RU2264950C1 | 
| FLYING VEHICLE LIFTING SURFACE TIP | 1993 | 
 | RU2063365C1 | 
| TIP | 2020 | 
 | RU2748824C1 | 
| FLYING VEHICLE WING | 2004 | 
 | RU2272745C1 | 
| MULTI-MEMBER TIP | 1997 | 
 | RU2118270C1 | 
Authors
Dates
1997-08-10—Published
1994-09-15—Filed