Podélná a stranová dynamická stabilita letounu

Longitudinal and Lateral Dynamic Stability

presentation

cs

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

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

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

aircraft testing in flight, flight measurement methodology, flight mechanics, stability, control, dynamic stability, longitudinal and lateral-directional motion

01.01.2004

Výzkumný a zkušební letecký ústav

Praha

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