A vertical-tailless aircraft (10) includes: a body (20) extending in a direction along an aircraft axis; a main wing (30) provided on a side surface (55) of the body (20); and a negative pressure generating portion (40) configured to generate negative pressure on the side surface (55) of a rear portion of the body (20) when the vertical-tailless aircraft (10) sideslips.
AIRCRAFT WITH NO VERTICAL TAIL
FLUGZEUG OHNE VERTIKALES LEITWERK
AÉRONEF SANS EMPANNAGE VERTICAL
2023-07-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
High-speed aircraft vertical tail and vertical tail optimization design method
European Patent Office | 2020
|Vertical tail buffeting of fighter aircraft
Online Contents | 2000
|Antenna assembly, vertical tail, horizontal tail, wing, aircraft and method
European Patent Office | 2021
|