A vertical-tailless aircraft includes a body, a main wing, and a negative pressure generating portion. The body extends in a direction along an aircraft axis and includes a front body and a rear body. The main wing is provided on a side surface of the body. The negative pressure generating portion is provided at the rear body and is configured to generate negative pressure on the side surface of the rear body in a case that the vertical-tailless aircraft sideslips.
VERTICAL-TAILLESS AIRCRAFT
25.02.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |