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Ein Abriß der Aeroelastizität

  • Chapter
Computerdynamik der Tragwerke

Zusammenfassung

Wir sind nun beim letzten Kapitel des dritten und abschließenden Bandes dieses Werkes angelangt. Nachdem wir über 35 Jahre hinweg das Studium der Luft- und Raumfahrttechnik an zwei Universitäten aufgebaut haben, betrachten wir es als eine konsequente Pflichtübung, aber auch als einen sentimentalen Epilog, in diesem letzten Kapitel auf ein ausgesprochen luftfahrtspezifisches Gebiet, das des Flatterns, einzugehen. Flattern stellt ein eigenartiges Phänomen des Zusammenwirkens der nichtkonservativen Luftkräfte mit der elastischen Struktur dar, das sowohl in statischer wie in dynamischer Hinsicht wirksam werden und im Grenzfall zu einer Katastrophe für das Flugzeug führen kann. In vorliegender Darstellung werden wir die aerodynamischen Kräfte, die wieder in Matrizenform angeordnet werden, als gegeben ansehen müssen, da unser Werk hauptsächlich auf die Struktur ausgerichtet ist.

Verfasser: John Argyris, Joachim Bühlmeier “῎Eπεα. πτερόεντα” “Geflügelte Worte” Homer, Ilias & Odyssee “Mετὰ σωφροσύνας οἴακι πειθοῦς” “We should steer with the rudder of self-control” Cercidas, Meliambs., iii, 1.15

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  1. Institut für Computer-Anwendungen, Universität Stuttgart, Deutschland

    Prof. em. Dr. Dr. h. c. mult. John Argyris F. Eng., F.R.S. & Dr. Ing. Hans-Peter Mlejnek (Gruppenleiter)

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  1. Prof. em. Dr. Dr. h. c. mult. John Argyris F. Eng., F.R.S.
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  2. Dr. Ing. Hans-Peter Mlejnek
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Argyris, J., Mlejnek, HP. (1997). Ein Abriß der Aeroelastizität. In: Computerdynamik der Tragwerke. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-89564-6_13

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