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Statements

Subject Item
n2:RIV%2F68407700%3A21220%2F11%3A00182031%21RIV13-GA0-21220___
rdf:type
skos:Concept n7:Vysledek
dcterms:description
Infrared camera, Particle Image Velocimetry, smokewire, tuft filaments and oil-flow visualization techniques were used for wind-tunnel and in-flight investigation of boundary layer separation, both stall and separation bubbles, related to the low-Reynolds numbers transition mechanism. Airfoils of Wortmann FX66 series and FX66 series wing-fuselage interaction, as well as modern airfoils and their wing-fuselage geometry were subject to study. The presence of previously identified structures in the CFD modelling, such as horse-shoe vortices, was confirmed in the flow. Wind-tunnels and in-flight measurements on sailplanes were carried out and effect of passive flow control devices Infrared camera, Particle Image Velocimetry, smokewire, tuft filaments and oil-flow visualization techniques were used for wind-tunnel and in-flight investigation of boundary layer separation, both stall and separation bubbles, related to the low-Reynolds numbers transition mechanism. Airfoils of Wortmann FX66 series and FX66 series wing-fuselage interaction, as well as modern airfoils and their wing-fuselage geometry were subject to study. The presence of previously identified structures in the CFD modelling, such as horse-shoe vortices, was confirmed in the flow. Wind-tunnels and in-flight measurements on sailplanes were carried out and effect of passive flow control devices
dcterms:title
VISUALIZATION OF BOUNDARY LAYER SEPARATION AND PASSIVE FLOW CONTROL ON AIRFOILS AND BODIES IN WIND-TUNNEL AND IN-FLIGHT EXPERIMENTS VISUALIZATION OF BOUNDARY LAYER SEPARATION AND PASSIVE FLOW CONTROL ON AIRFOILS AND BODIES IN WIND-TUNNEL AND IN-FLIGHT EXPERIMENTS
skos:prefLabel
VISUALIZATION OF BOUNDARY LAYER SEPARATION AND PASSIVE FLOW CONTROL ON AIRFOILS AND BODIES IN WIND-TUNNEL AND IN-FLIGHT EXPERIMENTS VISUALIZATION OF BOUNDARY LAYER SEPARATION AND PASSIVE FLOW CONTROL ON AIRFOILS AND BODIES IN WIND-TUNNEL AND IN-FLIGHT EXPERIMENTS
skos:notation
RIV/68407700:21220/11:00182031!RIV13-GA0-21220___
n7:predkladatel
n8:orjk%3A21220
n3:aktivita
n10:P
n3:aktivity
P(GA101/08/1112)
n3:dodaniDat
n18:2013
n3:domaciTvurceVysledku
n21:8931305
n3:druhVysledku
n23:D
n3:duvernostUdaju
n12:S
n3:entitaPredkladatele
n20:predkladatel
n3:idSjednocenehoVysledku
238568
n3:idVysledku
RIV/68407700:21220/11:00182031
n3:jazykVysledku
n4:eng
n3:klicovaSlova
vizualization; PIV; smokewire; tuft filaments; wind-tunnel; in-flight; airfoil; flow control
n3:klicoveSlovo
n5:vizualization n5:PIV n5:smokewire n5:wind-tunnel n5:airfoil n5:tuft%20filaments n5:in-flight n5:flow%20control
n3:kontrolniKodProRIV
[B2C2778FE037]
n3:mistoKonaniAkce
Moskva
n3:mistoVydani
Moskva
n3:nazevZdroje
Flow Visualization nad Image Processing (PSFVIP - 8)
n3:obor
n6:BK
n3:pocetDomacichTvurcuVysledku
1
n3:pocetTvurcuVysledku
6
n3:projekt
n13:GA101%2F08%2F1112
n3:rokUplatneniVysledku
n18:2011
n3:tvurceVysledku
Šimurda, D. Popelka, L. Uruba, V. Součková, N. Kuklová, J. Matějka, Milan
n3:typAkce
n22:WRD
n3:zahajeniAkce
2011-08-21+02:00
s:numberOfPages
6
n15:doi
10.1051/epjconf/20122501078
n11:hasPublisher
Lomonosov Moscow State University
n17:isbn
978-5-8279-0093-1
n19:organizacniJednotka
21220