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Description
  • Testováním v aerodynamickém tunelu byla provedena experimentální studie vlivu nánosu ledu z podchlazených kapek na aerodynamické vlastnosti profilu MS(1) 0313. Profil byl vybaven křidélkem. Námraza byla simulována lištou čtvrtkruhového průřezu s předním čelem kolmo k povrchu profilu. Byla zkoumány dva imitátory odlišných rozměrů, s výškou 1,33 % hloubky profilu a 2,25 % hloubky profilu. Imitátory byly umístěny v několika pozicích na horní straně profilu a hodnotil se jejich vliv na základní aerodynamické charakteristiky profilu, vztlak, odpor, moment a především závěsový moment křidélka. (cs)
  • An experimental investigation was conducted to study the aerodynamic effect of simulated supercooled large droplet ice accretion on a MS(1) 0313 aircraft airfoil by means of wind tunnel testing. The airfoil was equipped with an aileron. Ice accretion was simulated by a strip of a quadrantal section with front edge perpendicular to the surface of the airfoil. Two strips of different dimensions were examined, of the height of 1.33 % of chord and 2.25 % of chord, respectively. Every strip was positioned at several positions on the upper surface of the airfoil, and its influence on the basic aerodynamic characteristics of the airfoil was evaluated, i. e. the lift, drag, moment and first of all the hinge moment of the aileron.
  • An experimental investigation was conducted to study the aerodynamic effect of simulated supercooled large droplet ice accretion on a MS(1) 0313 aircraft airfoil by means of wind tunnel testing. The airfoil was equipped with an aileron. Ice accretion was simulated by a strip of a quadrantal section with front edge perpendicular to the surface of the airfoil. Two strips of different dimensions were examined, of the height of 1.33 % of chord and 2.25 % of chord, respectively. Every strip was positioned at several positions on the upper surface of the airfoil, and its influence on the basic aerodynamic characteristics of the airfoil was evaluated, i. e. the lift, drag, moment and first of all the hinge moment of the aileron. (en)
Title
  • Výzkum degradace výkonů na profilu s námrazou v aerodynamickém tunelu (cs)
  • Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils
  • Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils (en)
skos:prefLabel
  • Výzkum degradace výkonů na profilu s námrazou v aerodynamickém tunelu (cs)
  • Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils
  • Wind Tunnel Testing of Performance Degradation of Ice Contaminated Airfoils (en)
skos:notation
  • RIV/00010669:_____/00:00011612!RIV/2005/MPO/106695/N
http://linked.open.../vavai/riv/strany
  • 311.1;311.
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(PZ-D2/16)
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
  • 732791
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/00:00011612
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • aerodynamic characteristics;airfoil;aileron;ice accretion;wind tunnel;lift;drag;moment;hinge moment (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [C032FE5B93B1]
http://linked.open...v/mistoKonaniAkce
  • Harrogate, United Kingdom
http://linked.open...i/riv/mistoVydani
  • Harrogate, United Kingdom
http://linked.open...i/riv/nazevZdroje
  • Proceedings of 22nd International Congress of Aeronautical Sciences
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
  • Pátek, Zdeněk
  • Holl, Martin
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
number of pages
http://purl.org/ne...btex#hasPublisher
  • Neuveden
https://schema.org/isbn
  • 0-9533991-2-5
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