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Statische aeroelastische Probleme

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Grundlagen der Aeroelastik

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Zusammenfassung

Wie bereits in Kapitel 1 anhand der Funktionsdiagramme Abb. 1. 6 und 1. 7 gezeigt wurde, besteht die Problematik der analytischen Behandlung der statischen aeroelastischen Probleme von Auftriebssystemen in der Bestimmung des Einflusses der elastischen Verformung auf die stationäre aerodynamische Auftriebsverteilung und der Untersuchung der Stabilität des daraus resultierenden statischen Deformationsverhaltens. Die detaillierte Kenntnis dieser Zusammenhänge ist insbesondere bei Flugkonstruktionen von fundamentaler Bedeutung für die festigkeitsmäßige Auslegung und Gestaltung der Auftriebs- und Steuerflächen. Außerdem können die elastischen Deformatio-nen auch recht nachteilige Auswirkungen auf die statische Flugstabilität haben. Dasselbe gilt in übertragenem Sinne auch für die statische hydroelastische Stabilität und das Steuerungsverhalten von Tragflächenbooten.

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Authors and Affiliations

  1. Instituts für Aeroelastik, Deutschen Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e. V., Deutschland

    Privatdozent Dr.-Ing. Hans Wilhelm Försching (Direktor)

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  1. Privatdozent Dr.-Ing. Hans Wilhelm Försching
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© 1974 Springer-Verlag Berlin Heidelberg

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Försching, H.W. (1974). Statische aeroelastische Probleme. In: Grundlagen der Aeroelastik. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-48285-4_5

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  • DOI: https://doi.org/10.1007/978-3-642-48285-4_5

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-48286-1

  • Online ISBN: 978-3-642-48285-4

  • eBook Packages: Springer Book Archive

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