Počet záznamů: 1
Numerical simulation and experiments with the profile NACA 0012
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SYSNO ASEP 0377108 Druh ASEP A - Abstrakt Zařazení RIV Záznam nebyl označen do RIV Zařazení RIV Není vybrán druh dokumentu Název Numerical simulation and experiments with the profile NACA 0012 Tvůrce(i) Chládek, Štěpán (UT-L) RID
Zolotarev, Igor (UT-L) RID
Uruba, Václav (UT-L) RID, ORCIDZdroj.dok. Engineering Mechanics 2012. - Prague : ITAM AS CR, v. v. i., 2012 / Náprstek J. ; Fischer C. - ISBN 978-80-86246-39-0
S. 132-133Poč.str. 2 s. Akce Engineering Mechanics 2012 /18./ Datum konání 14.05.2012-17.05.2012 Místo konání Svratka Země CZ - Česká republika Typ akce WRD Jazyk dok. eng - angličtina Země vyd. CZ - Česká republika Klíč. slova aeroelastic ; flow-structure interaction ; identification Vědní obor RIV JU - Aeronautika, aerodynamika, letadla CEP GA101/09/1522 GA ČR - Grantová agentura ČR CEZ AV0Z20760514 - UT-L (2005-2011) Anotace This paper introduces the new model of the airfoil and describes both aeroelastic experiments and numerical simulation with the profile NACA 0012. The aeroelastic is the science which studies the flow-structure interaction. The flow field can cause change of the position of the solid body and the body due to the change of its position influences the flow field. Mathematical description of the interaction has to involve both the equations of the fluid dynamic and the equations of motion of the solid body. The first results will be presented from the measuring in the dynamic laboratory and from the measuring in the wind tunnel. The main aim of the experimental part of this research is to cause a self-oscillated motion of the airfoil and to measure the transient flow field during this motion. The numerical part should be identical with the experimental dates. Pracoviště Ústav termomechaniky Kontakt Marie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823 Rok sběru 2013
Počet záznamů: 1