The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

Result code in 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>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

The Longitudinal Dynamic Stability Flight Measurements of Light Aircraft

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 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.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

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

2003

Confidentiality

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

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2003

Issue of the periodical within the volume

3

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

6-9

UT code for WoS article

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EID of the result in the Scopus database

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