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  • The paper presents the results of a project which is focused on the design of the composite rods which are used in the rigid control system of aircraft. The idea of the project is to give a designer a new instrument for easier designing of composite rods. Composite rod calculation with a variable cross section is a fast and exact method how to obtain a rod with minimum weight. The calculation algorithm is divided into two parts. One for a composite rod with constant circular cross section and the second one for a composite rod with variable cross section. It is necessary to get maximum critical force, which means having critical force in every layer of the composite structure. The partial critical force is solved by means of an analytic method for the isotropic material. The result of the optimization calculation is the sum of partial critical forces for individual layers. The optimization criterion is the rod weight, optimized variables are rod diameter and thickness of the rod wall.
  • The paper presents the results of a project which is focused on the design of the composite rods which are used in the rigid control system of aircraft. The idea of the project is to give a designer a new instrument for easier designing of composite rods. Composite rod calculation with a variable cross section is a fast and exact method how to obtain a rod with minimum weight. The calculation algorithm is divided into two parts. One for a composite rod with constant circular cross section and the second one for a composite rod with variable cross section. It is necessary to get maximum critical force, which means having critical force in every layer of the composite structure. The partial critical force is solved by means of an analytic method for the isotropic material. The result of the optimization calculation is the sum of partial critical forces for individual layers. The optimization criterion is the rod weight, optimized variables are rod diameter and thickness of the rod wall. (en)
Title
  • Composite Rod Optimization Calculation
  • Composite Rod Optimization Calculation (en)
skos:prefLabel
  • Composite Rod Optimization Calculation
  • Composite Rod Optimization Calculation (en)
skos:notation
  • RIV/68407700:21220/10:00169572!RIV11-MSM-21220___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(1M0501)
http://linked.open...iv/cisloPeriodika
  • 3
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
  • 251662
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21220/10:00169572
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Rod; Optimization; Calculation (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • CZ - Česká republika
http://linked.open...ontrolniKodProRIV
  • [9067D914A7B7]
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
  • Jeřábek, Ivan
  • Stehlík, J.
issn
  • 1211-877X
number of pages
http://localhost/t...ganizacniJednotka
  • 21220
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