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Wind Tunnel Test of Whirl Flutter Aeroelastic Demonstrator

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F17%3AN0000017" target="_blank" >RIV/00010669:_____/17:N0000017 - isvavai.cz</a>

  • Result on the web

    <a href="https://arc.aiaa.org/doi/pdf/10.2514/6.2017-0635" target="_blank" >https://arc.aiaa.org/doi/pdf/10.2514/6.2017-0635</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.2514/6.2017-0635" target="_blank" >10.2514/6.2017-0635</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Wind Tunnel Test of Whirl Flutter Aeroelastic Demonstrator

  • Original language description

    This paper discusses the recent accomplishments in the testing of the W WING whirl flutter demonstrator. First, the paper gives a theoretical background on the whirl flutter phenomenon and outlines information about the demonstrator itself, past design and development activities and preparatory experiments including mass and stiffness measurements, modal tests and engine tests. The main focus is on the wind tunnel measurements. First and second experiments are described. The wind tunnel test description includes the test equipment and methodology as well as the test result assessment methodology and examples of the results. Finally, the outcome and future activities are outlined.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2017

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

  • ISSN

    0954-4100

  • e-ISSN

    2041-3025

  • Volume of the periodical

    233

  • Issue of the periodical within the volume

    3

  • Country of publishing house

    GB - UNITED KINGDOM

  • Number of pages

    9

  • Pages from-to

    969-977

  • UT code for WoS article

    000458991100015

  • EID of the result in the Scopus database

    2-s2.0-85017346693