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  • This paper presents the design and validation of a measurement system for aerodynamic characteristics of unmanned aerial vehicles. The largest modern unmanned aerial vehicles (UAV) have a wingspan of more than 30 m; the smallest UAVs can be carried in a backpack and operate at relatively low Reynolds numbers. An aerodynamic balance was designed in order to measure the lift, drag forces and pitching moment for different airfoils. During the design process, several aspects were analyzed in order to produce an efficient design and the balance was calibrated as well. Wind tunnel tests of a 2D NACA airfoil were performed to validate the aerodynamic measurement system. Finally, results of the wind tunnel tests were compared with references and found to be in good agreement.
  • This paper presents the design and validation of a measurement system for aerodynamic characteristics of unmanned aerial vehicles. The largest modern unmanned aerial vehicles (UAV) have a wingspan of more than 30 m; the smallest UAVs can be carried in a backpack and operate at relatively low Reynolds numbers. An aerodynamic balance was designed in order to measure the lift, drag forces and pitching moment for different airfoils. During the design process, several aspects were analyzed in order to produce an efficient design and the balance was calibrated as well. Wind tunnel tests of a 2D NACA airfoil were performed to validate the aerodynamic measurement system. Finally, results of the wind tunnel tests were compared with references and found to be in good agreement. (en)
Title
  • Design of precision aerodynamic balance for unmanned aerial vehicles
  • Design of precision aerodynamic balance for unmanned aerial vehicles (en)
skos:prefLabel
  • Design of precision aerodynamic balance for unmanned aerial vehicles
  • Design of precision aerodynamic balance for unmanned aerial vehicles (en)
skos:notation
  • RIV/68407700:21220/09:00159838!RIV11-MSM-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • S
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
  • 309701
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/09:00159838
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Aerodynamic; wing; lift; drag; forces (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [75F654354B08]
http://linked.open...v/mistoKonaniAkce
  • Liberec
http://linked.open...i/riv/mistoVydani
  • Liberec
http://linked.open...i/riv/nazevZdroje
  • Experimental Fluid Mechanics 2009
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Nožička, Jiří
  • Velazquez, Araque Luis
http://linked.open...vavai/riv/typAkce
http://linked.open...ain/vavai/riv/wos
  • 000276954300045
http://linked.open.../riv/zahajeniAkce
number of pages
http://purl.org/ne...btex#hasPublisher
  • Technická univerzita v Liberci
https://schema.org/isbn
  • 978-80-7372-538-9
http://localhost/t...ganizacniJednotka
  • 21220
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