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Assessment of flutter instability in simplified blade cascade using CFD based on discontinuous Galerkin method

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23520%2F17%3A43950558" target="_blank" >RIV/49777513:23520/17:43950558 - isvavai.cz</a>

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Assessment of flutter instability in simplified blade cascade using CFD based on discontinuous Galerkin method

  • Original language description

    The central target of the this paper is to present a flutter analysis of the so called simplified blade cascade in a fluid flow. The simplified blade cascade is formed by flat plates instead of real turbine blades. The approach to the flutter analysis is based on travelling wave mode, in which case the flat plates perform a kinematic harmonic motion, each with a different inter-blade phase angle. The aim of the simulations is to determine the aerodynamic damping coefficients caused by the aerodynamic forces acting on the flat plates, which show whether flutter occurs. Another approach to the flutter analysis that involves interaction of flat plates with the fluid flow is presented here. To this end the fluid-structure interaction algorithm is used. The resulting free vibration and natural inter-blade phase angle of the flat plates is analysed. The non-linear system of Favre-averaged Navier-Stokes equations in ALE formulation completed by the Spalart-Allmaras turbulence model was chosen as the mathematical model of a fluid flow. For the modelling of structure movement, the equation for harmonic oscillator was used. The simulations were performed using the developed in-house CFD software based on the discontinuous Galerkin method, which offers high order of accuracy.

  • Czech name

  • Czech description

Classification

  • Type

    O - Miscellaneous

  • CEP classification

  • OECD FORD branch

    20302 - Applied mechanics

Result continuities

  • Project

    <a href="/en/project/GA16-04546S" target="_blank" >GA16-04546S: Aero-elastic couplings and dynamic behaviour of rotational periodic bodies</a><br>

  • Continuities

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

Others

  • Publication year

    2017

  • Confidentiality

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