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Design and Development of New 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_____%2F14%3A%230001691" target="_blank" >RIV/00010669:_____/14:#0001691 - isvavai.cz</a>

  • Result on the web

    <a href="http://arc.aiaa.org/doi/abs/10.2514/6.2014-0678" target="_blank" >http://arc.aiaa.org/doi/abs/10.2514/6.2014-0678</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.2514/6.2014-0678" target="_blank" >10.2514/6.2014-0678</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Design and Development of New Whirl Flutter Aeroelastic Demonstrator

  • Original language description

    This paper deals with the design and development of the new whirl flutter aeroelastic demonstrator. The paper gives a theoretical background of the whirl flutter phenomenon and summarizes the whirl flutter occurrence in the aerospace practice. The secondpart is focused on the experimental research of the whirl flutter. At first the brief summary of past main developments in this field is provided. The main part deals with the new aeroelastic demonstrator "W-WING" designed and developed at the VZLU. Thedemonstrator represents the wing and engine of the twin turboprop commuter aircraft. Contrary to the most of past demonstrators it includes thrusting propeller. It allows the changes of the main structural parameters influencing the whirl flutter stability characteristics. The demonstrator is intended for the experimental investigations in the VZLU 3m-diameter low-speed wind tunnel. The results will be utilized for validation of analytical methods and software tools as well as in the fr

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

    <a href="/en/project/7E12035" target="_blank" >7E12035: Efficient Systems and Propulsion for Small Aircraft</a><br>

  • Continuities

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

Others

  • Publication year

    2014

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference Proceedings

  • ISBN

    978-1-62410-314-8

  • ISSN

  • e-ISSN

  • Number of pages

    14

  • Pages from-to

  • Publisher name

    American Institute of Aeronautics and Astronautics (AIAA)

  • Place of publication

    USA

  • Event location

    National Harbor, MD, USA

  • Event date

    Jan 1, 2014

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article