Numerical Study of Steady Transonic Flow over VELA (Very Efficient Large Aircraft)

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F10%3A00167232" target="_blank" >RIV/68407700:21220/10:00167232 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Numerical Study of Steady Transonic Flow over VELA (Very Efficient Large Aircraft)
Original language description
This study deals with numerical simulation of 3D steady inviscid flow around VELA. For the discretization of numerical fluxes, the well-known Roe Riemann Solver is used. To handle with time the implicit backward Euler is employed in order to accelerate the calculating time. The used program is just the first step on our way to develop efficient solver for unsteady viscous flow. In the end, some numerical results are presented together with a comparison of pressure coefficient Cp along three section. Ourresults are compared with results obtained by Fluent, StarCD and Edge. As you can see, we met in good agreement.
Czech name
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Czech description
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Project
<a href="/en/project/OC%20167" target="_blank" >OC 167: Numerical simulation in internal aerodynamics using LES or LES/RANS methods</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Topical Problems of Fluid Mechanics 2010 Proceedings
ISBN
978-80-87012-25-3
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
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Publisher name
Institute of Thermomechanics, AS CR, v.v.i.
Place of publication
Prague
Event location
Praha
Event date
Feb 10, 2010
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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