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Experimental Investigation of Propeller Aerodynamic Derivatives

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F25%3AN0000040" target="_blank" >RIV/00010669:_____/25:N0000040 - isvavai.cz</a>

  • Result on the web

    <a href="https://www.eucass.eu/component/docindexer/?id=6802&task=download" target="_blank" >https://www.eucass.eu/component/docindexer/?id=6802&task=download</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.13009/EUCASS2025-012" target="_blank" >10.13009/EUCASS2025-012</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Experimental Investigation of Propeller Aerodynamic Derivatives

  • Original language description

    The paper is focused on the experimental determination of the propeller aerodynamic derivatives that are used for the analysis of whirl flutter. Whirl flutter is a specific type of flutter instability that is driven by motion-induced unsteady aerodynamic propeller forces and moments acting in the propeller plane. To determine the forces and moments acting at the propeller disc, propeller aerodynamic derivatives are used. The analytical solution of derivatives is unreliable, and therefore, experimental validation of the selected derivatives is required. Paper describes the mechanical concept of the used demonstrator that represents a sting mounted nacelle with a motor and propeller with two degrees-of-freedom (engine pitch and yaw). The main focus is paid on the test including the list of the tested variants, methodology of testing and the data assessment. Finally, the examples of the results are provided.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    R - Projekt Ramcoveho programu EK

Others

  • Publication year

    2025

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    11th European Conference for Aero-Space Sciences (EuCASS), Conference Programme

  • ISBN

    978-80-87012-84-0

  • ISSN

    1805-8256

  • e-ISSN

  • Number of pages

    13

  • Pages from-to

    243-256

  • Publisher name

    European Conference for Aero-Space Sciences (EuCASS)

  • Place of publication

    Roma - Italy

  • Event location

    Roma - Italy

  • Event date

    Jan 1, 2025

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article