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The influence of structural damping on flutter characteristics of a small sport aircraft

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F11%3A00184546" target="_blank" >RIV/68407700:21220/11:00184546 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    The influence of structural damping on flutter characteristics of a small sport aircraft

  • Original language description

    Authors present the basic mathematical models of damping and principles of experimental determination of structural from the system frequency response. The specific method was applied on measurement of few types of small sport aircrafts. For some typicalmode shapes the. The applicability of the used method is discused for needs of flutter calculations of small aircraft.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>

  • Continuities

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

Others

  • Publication year

    2011

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Czech Aerospace

  • ISSN

    1211-877X

  • e-ISSN

  • Volume of the periodical

    2011

  • Issue of the periodical within the volume

    1

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    5

  • Pages from-to

    16-20

  • UT code for WoS article

  • EID of the result in the Scopus database