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
19.07.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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