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Description
  • This paper focuses on a suppression of the flow separation, which occurs on a deflected flap, by means of vortex generators (VG's). An airfoil NACA 63A421 with a simple flap and vane-type vortex generators were used. The investigation was carried out by using experimental and numerical methods. The data from the numerical simulation of the flapped airfoil without VG's control were used for the vortex generator design. Two sizes, two different shapes and various spacing of the vortex generators were tested. The flow past the airfoil was visualized through three methods, namely tuft filaments technique, oil and thermo camera visualization. The experiments were performed in closed circuit wind tunnels with closed and open test sections. The lift curves for both cases without and with vortex generators were acquired for a lift coefficient improvement determination. The improvement was achieved for several cases by means all of the applied methods.
  • This paper focuses on a suppression of the flow separation, which occurs on a deflected flap, by means of vortex generators (VG's). An airfoil NACA 63A421 with a simple flap and vane-type vortex generators were used. The investigation was carried out by using experimental and numerical methods. The data from the numerical simulation of the flapped airfoil without VG's control were used for the vortex generator design. Two sizes, two different shapes and various spacing of the vortex generators were tested. The flow past the airfoil was visualized through three methods, namely tuft filaments technique, oil and thermo camera visualization. The experiments were performed in closed circuit wind tunnels with closed and open test sections. The lift curves for both cases without and with vortex generators were acquired for a lift coefficient improvement determination. The improvement was achieved for several cases by means all of the applied methods. (en)
Title
  • VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION
  • VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION (en)
skos:prefLabel
  • VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION
  • VISUALIZATION OF FLOW SEPARATION AND CONTROL BY VORTEX GENERATORS ON AN SINGLE FLAP IN LANDING CONFIGURATION (en)
skos:notation
  • RIV/68407700:21220/10:00181055!RIV12-GA0-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(1M06031), P(GA101/08/1112), P(GA103/09/0977), P(GAP101/10/1230), Z(AV0Z20760514)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 295816
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/10:00181055
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • flow control; vortex generator; landing configuration (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [A37F3B87D9D0]
http://linked.open...v/mistoKonaniAkce
  • Liberec
http://linked.open...i/riv/mistoVydani
  • Liberec
http://linked.open...i/riv/nazevZdroje
  • EXPERIMENTAL FLUID MECHANICS 2010
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Kuklová, J.
  • Matějka, Milan
  • Popelka, L.
  • Součková, Natálie
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • Technická univerzita v Liberci
https://schema.org/isbn
  • 978-80-7372-670-6
http://localhost/t...ganizacniJednotka
  • 21220
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