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Description
| - The phenomenon of in-flight icing may affect all types of aircraft. Aircraft icing causes iced airfoils aerodynamic characteristics degradation. From aerodynamics viewpoint, when compared to wings without ice, wings with ice indicate decreased maximum lift, increased drag, changes in pressure distribution, stall occurring at markedly lower angles of attack, and so increased stall speed. Thus, it is important to understand the different ice shapes that can form on the wings and how they affect aerodynamics. The two-dimensional Navier-Stokes CFD simulation was used for study of aerodynamic performance of iced airfoils the geometry of whose is rather complicated. Results are compared with the wind tunnel testing on models with artificial ice shapes in dry air.
- The phenomenon of in-flight icing may affect all types of aircraft. Aircraft icing causes iced airfoils aerodynamic characteristics degradation. From aerodynamics viewpoint, when compared to wings without ice, wings with ice indicate decreased maximum lift, increased drag, changes in pressure distribution, stall occurring at markedly lower angles of attack, and so increased stall speed. Thus, it is important to understand the different ice shapes that can form on the wings and how they affect aerodynamics. The two-dimensional Navier-Stokes CFD simulation was used for study of aerodynamic performance of iced airfoils the geometry of whose is rather complicated. Results are compared with the wind tunnel testing on models with artificial ice shapes in dry air. (en)
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Title
| - Performance Degradation of Iced Airfoils
- Performance Degradation of Iced Airfoils (en)
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skos:prefLabel
| - Performance Degradation of Iced Airfoils
- Performance Degradation of Iced Airfoils (en)
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skos:notation
| - RIV/60162694:G43__/09:#0003005!RIV10-MO0-G43_____
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/60162694:G43__/09:#0003005
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - Aerodynamics; Aircraft icing; Wind tunnel testing (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...ontrolniKodProRIV
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http://linked.open...v/mistoKonaniAkce
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http://linked.open...i/riv/mistoVydani
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http://linked.open...i/riv/nazevZdroje
| - ICMT’09, International Conference on Military Technologies
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
| - Horák, Vladimír
- ROZEHNAL, DALIBOR
- GAŠPAROVIČ, PETER
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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http://linked.open...n/vavai/riv/zamer
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number of pages
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http://purl.org/ne...btex#hasPublisher
| - Faculty of Military Technology, University of Defence
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https://schema.org/isbn
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http://localhost/t...ganizacniJednotka
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