The present invention refers to aircraft tail surfaces and more particularly to a configuration of an aircraft tail surface (1) with a single protrusion (3) for improving air flow control with no or negligible drag penalty.
AIRCRAFT TAIL SURFACE
FLUGZEUGHECKFLÄCHE
SURFACE ARRIÈRE D'AÉRONEF
2025-05-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft tail and aircraft comprising such aircraft tail
European Patent Office | 2024
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