Longitudinal and Lateral Dynamic Stability

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F04%3APU48266" target="_blank" >RIV/00216305:26210/04:PU48266 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

čeština

Original language name

Podélná a stranová dynamická stabilita letounu

Original language description

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 thisresearch, is the two-seat all-metal motor glider L-13 SE Vivat

Czech name

Podélná a stranová dynamická stabilita letounu

Czech description

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 thisresearch, is the two-seat all-metal motor glider L-13 SE Vivat

Type

A - Audiovisual production

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2004

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

ISBN

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Place of publication

Praha

Publisher/client name

Výzkumný a zkušební letecký ústav

Version

neuvedeno

Carrier ID

neuvedeno