Fast Estimation of Classical Flutter Stability of Turbine Blade by Reduced CFD Modelling

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F20%3A00543123" target="_blank" >RIV/61388998:_____/20:00543123 - isvavai.cz</a>

Výsledek na webu

<a href="https://www.taylorfrancis.com/books/oa-edit/10.1201/9781003132639/12th-international-conference-vibrations-rotating-machinery" target="_blank" >https://www.taylorfrancis.com/books/oa-edit/10.1201/9781003132639/12th-international-conference-vibrations-rotating-machinery</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1201/9781003132639" target="_blank" >10.1201/9781003132639</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Fast Estimation of Classical Flutter Stability of Turbine Blade by Reduced CFD Modelling

Popis výsledku v původním jazyce

The paper presents a medium fidelity reduced ordered numerical model for the calculation of aeroelastic stability diagram of 3D blade cascade of low pressure stage of steam turbine. The aeroelastic stability in steam turbine blades are calculated for the classical flutter problem. The calculation of the stability diagram for the problem of classical flutter is evaluated with assumption of running waves. Running waves will be simulated by the inter-blade phase shift approach between the blades in the cascade. Panel method based boundary element type flow solver is employed for calculation of unsteady aerodynamic forces and model the flow flied. This method is good compromise of speed and accuracy for the estimation of the stability of the blades on a classical flutter. The estimated results are compared with experimental and the high fidelity computational fluid dynamic model data.n

Název v anglickém jazyce

Fast Estimation of Classical Flutter Stability of Turbine Blade by Reduced CFD Modelling

Popis výsledku anglicky

The paper presents a medium fidelity reduced ordered numerical model for the calculation of aeroelastic stability diagram of 3D blade cascade of low pressure stage of steam turbine. The aeroelastic stability in steam turbine blades are calculated for the classical flutter problem. The calculation of the stability diagram for the problem of classical flutter is evaluated with assumption of running waves. Running waves will be simulated by the inter-blade phase shift approach between the blades in the cascade. Panel method based boundary element type flow solver is employed for calculation of unsteady aerodynamic forces and model the flow flied. This method is good compromise of speed and accuracy for the estimation of the stability of the blades on a classical flutter. The estimated results are compared with experimental and the high fidelity computational fluid dynamic model data.n

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20302 - Applied mechanics

Projekt

<a href="/cs/project/TN01000007" target="_blank" >TN01000007: Národní centrum pro energetiku</a><br>

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2020

Kód důvěrnosti údajů

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

Název statě ve sborníku

12th International Conference on Vibrations in Rotating Machinery : VIRM 2020

ISBN

978-0-367-67742-8

ISSN

—

e-ISSN

—

Počet stran výsledku

10

Strana od-do

226-239

Název nakladatele

Taylor & Francis Group

Místo vydání

London

Místo konání akce

on-line

Datum konání akce

14. 10. 2020

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

—