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Description
| - Příspěvek pojednává o aeroelastické optimalizaci. Podává základní přehled teoretických aspektů se zřetelem k problematice aeroelasticity. Hlavní část popisuje optimalizaci tuhostních charakteristik křídla letounu s cílem dosažení aeroelastické stability při průkazné rychlosti. Hlavní problém představuje plnění okrajové nádrže palivem, které způsobuje výrazné změny modálních a flatrových charakteristik konstrukce. Cílem úlohy je dosažení požadované úrovně stability pro všechny úrovně plnění okrajové nádrže. (cs)
- Paper deals with aeroelastic optimization. It gives a summary of theory with special regard to the aeroelasticity. Main part describes optimization of the aircraft wing stiffness characteristics to ensure the flutter stability below the certification speed. The problem is represented by the wing tip tank filling, which causes significant change of the modal characteristics and so the flutter stability characteristics. The task aim is to ensure flutter stability below the certification speed for whole range of the tip tank filling.
- Paper deals with aeroelastic optimization. It gives a summary of theory with special regard to the aeroelasticity. Main part describes optimization of the aircraft wing stiffness characteristics to ensure the flutter stability below the certification speed. The problem is represented by the wing tip tank filling, which causes significant change of the modal characteristics and so the flutter stability characteristics. The task aim is to ensure flutter stability below the certification speed for whole range of the tip tank filling. (en)
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Title
| - Optimization of the Commuter Aircraft Wing stiffness Characteristics Considering Requirement of Aeroelastic Stability at the Certification Speed
- Optimalizace tuhostních charakteristik křídla dopravního letounu s ohledem na požadavek aeroelastické stability při průkazné rychlosti (cs)
- Optimization of the Commuter Aircraft Wing stiffness Characteristics Considering Requirement of Aeroelastic Stability at the Certification Speed (en)
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skos:prefLabel
| - Optimization of the Commuter Aircraft Wing stiffness Characteristics Considering Requirement of Aeroelastic Stability at the Certification Speed
- Optimalizace tuhostních charakteristik křídla dopravního letounu s ohledem na požadavek aeroelastické stability při průkazné rychlosti (cs)
- Optimization of the Commuter Aircraft Wing stiffness Characteristics Considering Requirement of Aeroelastic Stability at the Certification Speed (en)
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skos:notation
| - RIV/00010669:_____/07:#0000632!RIV08-MPO-00010669
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http://linked.open.../vavai/riv/strany
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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/00010669:_____/07:#0000632
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - aeroelasticity, flutter, aeroelasatic optimization (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
| - Engineering Mechanics 2007, National Conference with International Participation
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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...vavai/riv/projekt
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http://linked.open...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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number of pages
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http://purl.org/ne...btex#hasPublisher
| - Association for Engineering Mechanics, Institute of solid Mechanics, Mechatronics and Biomechanics, Institute of Theoretical and Applied Mechanics, etc.
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https://schema.org/isbn
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is http://linked.open...avai/riv/vysledek
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