FIELD: aeronautical engineering; aircraft aerodynamic configuration. SUBSTANCE: aircraft has two- wing combination: one wing is located in front of CG and other located after CG and aerodynamic center of wing combination coincides with aircraft CG. EFFECT: enhanced efficiency. 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| TRAINER AEROPLANE | 1996 |
|
RU2100251C1 |
| SUPERSONIC AIRCRAFT OF NORMAL CONFIGURATION WITH REAR POSITION OF CENTRE OF MASS AND BEARING STABILIZER | 2024 |
|
RU2835242C1 |
| AIRCRAFT | 1993 |
|
RU2087384C1 |
| VTOL AIRCRAFT | 2006 |
|
RU2350510C2 |
| AIRCRAFT-TRIPLANE | 1998 |
|
RU2172706C2 |
| AIRCRAFT WITH OSCILLATING SLATS | 2010 |
|
RU2457154C2 |
| METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD | 2010 |
|
RU2539443C2 |
| AIRCRAFT | 2014 |
|
RU2577824C1 |
| FLYING WING TYPE AIRCRAFT | 2019 |
|
RU2744692C2 |
