About: Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes     Goto   Sponge   NotDistinct   Permalink

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Description
  • Je popsán Lagrangeův model flatrových rovnic vztlakové plochy se dvěma kormidly pro modální charakteristiky nosné plochy s pevnými kormidly a izolovaných kormidel. Je prezentována kompilace maticového schématu pro výpočet vlastních čísel a naznačen výpočtový postup %22p-k%22 modelu pro stanovení frekvencí a tlumení v závislosti na rychlosti letu s nestacionárním Theodorseným aerodynamický modelem tenkého profilu s klapkou a zjednodušenými vztahy pro výpočet zobecněných hmot. (cs)
  • Lagrange´s model of flutter equation of a lift surface with two control surfaces based on modal characteristics of the lift surface with fixed control surfaces and isolated control surfaces is described. It is presented a matrix scheme compilation for a calculation of eigenvalues and outlined the %22p-k%22 model type for calculation of frequencies and damping versus flight speed for non-stacionary Theodorsen´s aerodynamic model of thin profile with flap and simplified relations for calculations of generalized masses.
  • Lagrange´s model of flutter equation of a lift surface with two control surfaces based on modal characteristics of the lift surface with fixed control surfaces and isolated control surfaces is described. It is presented a matrix scheme compilation for a calculation of eigenvalues and outlined the %22p-k%22 model type for calculation of frequencies and damping versus flight speed for non-stacionary Theodorsen´s aerodynamic model of thin profile with flap and simplified relations for calculations of generalized masses. (en)
Title
  • Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes
  • Výpočtový model flatru s zolovanými modálními charakteristikami kormidel pro malé sportovní letouny (cs)
  • Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes (en)
skos:prefLabel
  • Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes
  • Výpočtový model flatru s zolovanými modálními charakteristikami kormidel pro malé sportovní letouny (cs)
  • Flutter Calculation Model with Isolated Modal Characteristics of Control Surfaces for Small Sport Airplanes (en)
skos:notation
  • RIV/68407700:21220/08:02150700!RIV09-MSM-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(1M0501)
http://linked.open...iv/cisloPeriodika
  • 2
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
  • 368247
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/08:02150700
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • aeroelasticity; empennage flutter; flutter analyzes; flutter characteristics; flutter equations; generalized aerodynamic forces; generalized masses; wing flutter (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • CZ - Česká republika
http://linked.open...ontrolniKodProRIV
  • [3490E947E978]
http://linked.open...i/riv/nazevZdroje
  • Czech Aerospace
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...v/svazekPeriodika
  • 2008
http://linked.open...iv/tvurceVysledku
  • Slavík, Svatomír
  • Weigel, Karel
issn
  • 1211-877X
number of pages
http://localhost/t...ganizacniJednotka
  • 21220
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