Laminar-Turbulent Boundary Layer Transition Modelling for Turbomachinery Flows.

Result code in IS VaVaI

RIV/00010669:_____/10:#0001001 - isvavai.cz

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Laminar-Turbulent Boundary Layer Transition Modelling for Turbomachinery Flows.

Original language description

A modified algebraic model of the laminar-turbulent bypass transition was implemented into the in-house numerical code for the simulation of the compressible turbulent flow using the RANS equation closed by the two-equation k-? TNT turbulence model. Themodel was verified by the ERCOFTAC test cases for various boundary-layer flows and applied for the simulaton of the transitional flow in turbine blade cascades.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

BK - Liquid mechanics

OECD FORD branch

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Project

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2010

Confidentiality

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

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

4/2010

Issue of the periodical within the volume

4

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

3

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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