About: X-DIA Demonstrator Aeroelastic Test – Design, Analysis And Model Wind Tunnel Support Tuning     Goto   Sponge   NotDistinct   Permalink

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  • Předkládaný článek pojednává o přípravné fázi aeroelastického experimentu demonstrátoru X-DIA. Článek se soustředí na vývoj, konstrukci a výrobu nových kompozitních předkřídel, dále na výpočty, zejména aroelastické, provedené na soustavě částečného modelu X-DA (statická aeroelasticita, flatr, dynamická odezva) a konečně na optimalizační studii závěsu modelu v aerodynamickém tunelu. Výpočty byly provedeny pomocí programového systému MSC.NASTRAN. (cs)
  • Submitted paper deals with preparation of the X-DIA aeroelastic demonstrator component wind tunnel tests. The paper is focused on design, analysis and manufacturing of new composite foreplanes, FE analyses of the X-DIA Component Model (static aeroelasticity, flutter, dynamic responses) and optimization study of the demonstrator wind tunnel support device. Analyses were performed by means of the MSC.NASTRAN program system.
  • Submitted paper deals with preparation of the X-DIA aeroelastic demonstrator component wind tunnel tests. The paper is focused on design, analysis and manufacturing of new composite foreplanes, FE analyses of the X-DIA Component Model (static aeroelasticity, flutter, dynamic responses) and optimization study of the demonstrator wind tunnel support device. Analyses were performed by means of the MSC.NASTRAN program system. (en)
Title
  • X-DIA Demonstrator Aeroelastic Test – Design, Analysis And Model Wind Tunnel Support Tuning
  • X-DIA Demonstrator Aeroelastic Test – Design, Analysis And Model Wind Tunnel Support Tuning (en)
  • Aeroelastický test demonstrátoru X-DIA – Konstrukce, analýza a úpravy zástavby modelu v aerodynamickém tunelu (cs)
skos:prefLabel
  • X-DIA Demonstrator Aeroelastic Test – Design, Analysis And Model Wind Tunnel Support Tuning
  • X-DIA Demonstrator Aeroelastic Test – Design, Analysis And Model Wind Tunnel Support Tuning (en)
  • Aeroelastický test demonstrátoru X-DIA – Konstrukce, analýza a úpravy zástavby modelu v aerodynamickém tunelu (cs)
skos:notation
  • RIV/00010669:_____/06:#0000192!RIV07-MSM-00010669
http://linked.open.../vavai/riv/strany
  • 357-366
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MSM0001066903)
http://linked.open...iv/cisloPeriodika
  • No.5
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
  • 509148
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/06:#0000192
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • aeroelasticity; flutter; dynamic response; aeroelastic tests; active control; all-movable; foreplane (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • CZ - Česká republika
http://linked.open...ontrolniKodProRIV
  • [230F8C6566A1]
http://linked.open...i/riv/nazevZdroje
  • Engineering Mechanics
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...v/svazekPeriodika
  • Vol. 13
http://linked.open...iv/tvurceVysledku
  • Čečrdle, Jiří
http://linked.open...n/vavai/riv/zamer
issn
  • 1210-2717
number of pages
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