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Description
  • This paper deals with the design and development of the new whirl flutter aeroelastic demonstrator. The paper gives a theoretical background of the whirl flutter phenomenon and summarizes the whirl flutter occurrence in the aerospace practice. The second part is focused on the experimental research of the whirl flutter. At first the brief summary of past main developments in this field is provided. The main part deals with the new aeroelastic demonstrator %22W-WING%22 designed and developed at the VZLU. The demonstrator represents the wing and engine of the twin turboprop commuter aircraft. Contrary to the most of past demonstrators it includes thrusting propeller. It allows the changes of the main structural parameters influencing the whirl flutter stability characteristics. The demonstrator is intended for the experimental investigations in the VZLU 3m-diameter low-speed wind tunnel. The results will be utilized for validation of analytical methods and software tools as well as in the frame of the research projects.
  • This paper deals with the design and development of the new whirl flutter aeroelastic demonstrator. The paper gives a theoretical background of the whirl flutter phenomenon and summarizes the whirl flutter occurrence in the aerospace practice. The second part is focused on the experimental research of the whirl flutter. At first the brief summary of past main developments in this field is provided. The main part deals with the new aeroelastic demonstrator %22W-WING%22 designed and developed at the VZLU. The demonstrator represents the wing and engine of the twin turboprop commuter aircraft. Contrary to the most of past demonstrators it includes thrusting propeller. It allows the changes of the main structural parameters influencing the whirl flutter stability characteristics. The demonstrator is intended for the experimental investigations in the VZLU 3m-diameter low-speed wind tunnel. The results will be utilized for validation of analytical methods and software tools as well as in the frame of the research projects. (en)
Title
  • Design and Development of New Whirl Flutter Aeroelastic Demonstrator
  • Design and Development of New Whirl Flutter Aeroelastic Demonstrator (en)
skos:prefLabel
  • Design and Development of New Whirl Flutter Aeroelastic Demonstrator
  • Design and Development of New Whirl Flutter Aeroelastic Demonstrator (en)
skos:notation
  • RIV/00010669:_____/14:#0001691!RIV15-MSM-00010669
http://linked.open...avai/riv/aktivita
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  • P(7E12035)
http://linked.open...vai/riv/dodaniDat
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  • 10402
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  • RIV/00010669:_____/14:#0001691
http://linked.open...riv/jazykVysledku
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  • Aeroelastic Experiment; Whirl Flutter; W-WING (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [FEB0937B25B7]
http://linked.open...v/mistoKonaniAkce
  • National Harbor, MD, USA
http://linked.open...i/riv/mistoVydani
  • USA
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  • 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference Proceedings
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http://linked.open...iv/tvurceVysledku
  • Maleček, Jaromír
  • Čečrdle, Jiří
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
number of pages
http://bibframe.org/vocab/doi
  • 10.2514/6.2014-0678
http://purl.org/ne...btex#hasPublisher
  • American Institute of Aeronautics and Astronautics (AIAA)
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  • 978-1-62410-314-8
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