Rotor-Stator Interaction Using the Edge Solver

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001465" target="_blank" >RIV/00010669:_____/12:#0001465 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.czaerospace.eu/en/2012-3-45.html" target="_blank" >http://www.czaerospace.eu/en/2012-3-45.html</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Rotor-Stator Interaction Using the Edge Solver

Popis výsledku v původním jazyce

The subject of this paper is the numerical solution of rotor-stator configurations (compressors, turbines, fans) and the possibilities of simulation of flow through the common interface, which is represented by a pair of boundaries. Their connection is the subject of this study. Simplified version suitable also for steady state computations is represented by the Mixing Plane model, where all the quantities are averaged in the circumferential direction. More accurate Sliding Mesh approach, based on interpolation of quantities between boundaries, is discussed in more detail. The EDGE solver was used and the Sliding Mesh model was implemented by the author. The main ideas of implementation and few model problems used for testing are presented.

Název v anglickém jazyce

Rotor-Stator Interaction Using the Edge Solver

Popis výsledku anglicky

The subject of this paper is the numerical solution of rotor-stator configurations (compressors, turbines, fans) and the possibilities of simulation of flow through the common interface, which is represented by a pair of boundaries. Their connection is the subject of this study. Simplified version suitable also for steady state computations is represented by the Mixing Plane model, where all the quantities are averaged in the circumferential direction. More accurate Sliding Mesh approach, based on interpolation of quantities between boundaries, is discussed in more detail. The EDGE solver was used and the Sliding Mesh model was implemented by the author. The main ideas of implementation and few model problems used for testing are presented.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2012

Kód důvěrnosti údajů

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

Název periodika

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Svazek periodika

3/2012

Číslo periodika v rámci svazku

3

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

4

Strana od-do

14-17

Kód UT WoS článku

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EID výsledku v databázi Scopus

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