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KOUŘIL, M.; JEBÁČEK, I.; Prokš, M.
Originální název
The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft
Anglický název
Druh
Článek recenzovaný mimo WoS a Scopus
Originální abstrakt
The dynamic stability control presents one of the important parts of flight characteristics analysis of design atmospheric aircraft. The dynamic stability calculations, following aircraft from its primary design, have a great influence on the final aircraft appearance. The suitability of proposed aircraft design and possible modifications will appear just during the flight tests. The results of flight tests are used for the verification of applied theory and for the verification of designed aircraft stability and control as well. This paper presents the issue of flight measurement and theory calculations of longitudinal dynamic stability. It is dealing in detail with comparison of performed flight measurements and computations. The aircraft, mainly supporting this research, is the two-seat all-metal motor glider L-13 SE Vivat.
Anglický abstrakt
Klíčová slova
Aerodynamics, mechanics of flight, flight-tests, dynamic stability, flight characteristics
Klíčová slova v angličtině
Autoři
Vydáno
21.11.2003
Nakladatel
VZLÚ, a.s.
Místo
Praha
Kniha
Letecký zpravodaj
ISSN
1211-877X
Periodikum
Svazek
2003
Číslo
3
Stát
Česká republika
Strany od
6
Strany počet
4
BibTex
@article{BUT41950, author="Martin {Kouřil} and Ivo {Jebáček}", title="The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft", journal="Letecký zpravodaj", year="2003", volume="2003", number="3", pages="4", issn="1211-877X" }