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KOUŘIL, M.
Original Title
Podélná a stranová dynamická stabilita letounu
English Title
Longitudinal and Lateral Dynamic Stability
Type
presentation
Language
Czech
Original Abstract
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 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
English abstract
Keywords
aircraft testing in flight, flight measurement methodology, flight mechanics, stability, control, dynamic stability, longitudinal and lateral-directional motion
Authors
Released
1. 1. 2004
Publisher
Výzkumný a zkušební letecký ústav
Location
Praha
Pages from
55
Pages to
Pages count
1
BibTex
@misc{BUT63331, author="Martin {Kouřil}", title="Podélná a stranová dynamická stabilita letounu", year="2004", series="neuvedeno", edition="1", pages="1", publisher="Výzkumný a zkušební letecký ústav", address="Praha", note="presentation" }