Numerical Solution of 2D and 3D Transonic Flows over an Airfoil and a Wing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A02094163" target="_blank" >RIV/68407700:21220/03:02094163 - isvavai.cz</a>
Alternative codes found
RIV/68407700:21110/03:02094163
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 2D and 3D Transonic Flows over an Airfoil and a Wing
Original language description
This work presents results of numerical solution of transonic flows over 2D airfoils and 3D wings. Two different numerical methods were developed. The second method was used to solve 2D transonic turbulent flows with k-omega turbulent model over RAE 2822airfoil and also 3D transonic inviscid flows over a wing or wing-body combination. Numerical results were compared with experimental results of ARTI Prague.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
BA - General mathematics
OECD FORD branch
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Result continuities
Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2003
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
IUTAM Symposium Transsonicum IV, Book of Abstracts
ISBN
1-4020-1608-5
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
211-216
Publisher name
DLR
Place of publication
Göttingen
Event location
Göttingen
Event date
Sep 2, 2002
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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