The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU41982" target="_blank" >RIV/00216305:26210/03:PU41982 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

Popis výsledku v původním jazyce

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 staability 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.

Název v anglickém jazyce

The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

Popis výsledku anglicky

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 staability 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.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/LN00B051" target="_blank" >LN00B051: Centrum leteckého a kosmického výzkumu (CLKV)</a><br>

Návaznosti

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

Rok uplatnění

2003

Kód důvěrnosti údajů

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

Název periodika

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Svazek periodika

2003

Číslo periodika v rámci svazku

3

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

6-9

Kód UT WoS článku

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EID výsledku v databázi Scopus

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