Numerical Solution of Compressible Steadz Flows around the NACA 0012 Airfoil
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F13%3A00205464" target="_blank" >RIV/68407700:21220/13:00205464 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.1051/epjconf/20134501121" target="_blank" >http://dx.doi.org/10.1051/epjconf/20134501121</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/epjconf/20134501121" target="_blank" >10.1051/epjconf/20134501121</a>
Alternative languages
Result language
angličtina
Original language name
Numerical Solution of Compressible Steadz Flows around the NACA 0012 Airfoil
Original language description
The article presents results of numerical solution of subsonic and transonic flows described by the system of Navier-Stokes equations in 2D laminar flows around the NACA 0012 airfoil. Authors used Runge-Kutta method to numerically solve the flow around the NACA 0012 airfoil.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
BA - General mathematics
OECD FORD branch
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Result continuities
Project
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Continuities
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Others
Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
EPJ Web of Conferences
ISSN
2100-014X
e-ISSN
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Volume of the periodical
45
Issue of the periodical within the volume
45
Country of publishing house
FR - FRANCE
Number of pages
4
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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