Numerical Solution of Compressible Steady 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%2F12%3A00193709" target="_blank" >RIV/68407700:21220/12:00193709 - isvavai.cz</a>
Alternative codes found
RIV/46747885:24210/12:#0002698
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Numerical Solution of Compressible Steady Flows Around the NACA 0012 Airfoil
Original language description
The article presents results of a numerical solution of subsonic and transonic flows described by the system of Euler equations in 2D flows around the NACA 0012 airfoil. Authors used Runge-Kutta method to numerically solve the flows around the NACA 0012airfoil.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
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
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Power system, Engineering, Thermodynamics & Fluid flow 2012
ISBN
978-80-261-0113-0
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
1-4
Publisher name
Západočeská univerzita v Plzni
Place of publication
Plzeň
Event location
Srní
Event date
Jun 13, 2012
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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