Applied result detail

Zakonceni kridla typu winglet pro lehky letoun

POPELA, R.; ZIKMUND, P.

Original Title

Zakonceni kridla typu winglet pro lehky letoun

English Title

Winglet for light aircraft

Type

Prototype

Abstract

Specificke zakonceni kridla typu winglet, ktere snizuje indukovany odpor kridla. Material kompozit. Winglet byl navrzen pro letouny kategorie Ul, LSA a CS-VLA. Pro vybrane kridlo snizuje indukovany odpor kridla od soucinitele vztlaku 0,25.

Abstract in English

Winglet designed specifically for UL, LSA and CS-VLA aircraft categories. GFRP structure. The device reduces induced drag of wing (respectivelly whole aircraft) from lift coefficient around 0.25 and improves its gliding ratio and climb performance.

Keywords

winglet, CS-VLA, UL, LSA, indukovany odpor

Key words in English

winglet, CS-VLA, UL, LSA, aircraft, induced drag

Location

Letecky ustav FSI VUT v Brne

Possibilities of use

only the provider uses the result

Licence fee

Use of the result by another entity is possible without acquiring a license (the result is not licensed)