Numerical solution of inviscid and viscous laminar and turbulent flow around the airfoil

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F16%3A00333336" target="_blank" >RIV/68407700:21220/16:00333336 - isvavai.cz</a>

Result on the web

<a href="http://dx.doi.org/10.1051/epjconf/201611402109" target="_blank" >http://dx.doi.org/10.1051/epjconf/201611402109</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1051/epjconf/201611402109" target="_blank" >10.1051/epjconf/201611402109</a>

Result language

angličtina

Original language name

Numerical solution of inviscid and viscous laminar and turbulent flow around the airfoil

Original language description

This work deals with the 2D numerical solution of inviscid compressible flow and viscous compressible laminar and turbulent flow around the profile. In a case of turbulent flow algebraic Baldwin-Lomax model is used and compared with Wilcox k-omega model. Calculations are done for NACA 0012 and RAE 2822 airfoil profile for the different angles of upstream flow. Numerical results are compared and discussed with experimental data.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

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OECD FORD branch

20304 - Aerospace engineering

Project

<a href="/en/project/GAP101%2F12%2F1271" target="_blank" >GAP101/12/1271: Effect of complex boundary conditions on the laminar/turbulent transition</a><br>

Continuities

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

Publication year

2016

Confidentiality

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

Article name in the collection

EPJ Web of Conferences

ISBN

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ISSN

2100-014X

e-ISSN

2100-014X

Number of pages

6

Pages from-to

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Publisher name

EDP Sciences

Place of publication

Les Ulis

Event location

Praha

Event date

Nov 17, 2015

Type of event by nationality

WRD - Celosvětová akce

UT code for WoS article

000400395300111