This presentation (23 slides) describes a program, aimed at developing design guidelines for viscoelastic damping applied to skin-stringer-frame type aerospace structure. Periodic structure type response models developed as a first part of the program are discussed. Two procedures for assigning values of the damping parameters required in these models are presented. Results of test efforts to develop and verify the damping parameter assignment procedure and response prediction models are also discussed. The current status of these efforts is: (1) Response models are yielding predictions in agreement with test results; and (2) The damping parameter assignment procedures are working, but more work is needed to bring them up to the confidence level of the response models. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Integrated Damped Fuselage Structure


    Beteiligte:
    L. M. Butzel (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Fuselage for an aircraft with fuselage-integrated tailplane

    STANGL WOLFGANG / OSTERHUBER ROBERT / ERNSTBERGER PHILIPP | Europäisches Patentamt | 2023

    Freier Zugriff

    FUSELAGE FOR AN AIRCRAFT WITH FUSELAGE-INTEGRATED TAILPLANE

    STANGL WOLFGANG / OSTERHUBER ROBERT / ERNSTBERGER PHILIPP | Europäisches Patentamt | 2023

    Freier Zugriff

    FUSELAGE FOR AN AIRCRAFT WITH FUSELAGE-INTEGRATED TAILPLANE

    STANGL WOLFGANG / OSTERHUBER ROBERT / ERNSTBERGER PHILIPP | Europäisches Patentamt | 2025

    Freier Zugriff

    Fuselage skeleton structure, fuselage and aircraft

    XU JINHAO / ZHANG XIANG / LI JIANING | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT FUSELAGE WITH INTEGRATED POWER-ABSORBING STRAINING STRUCTURE AND AIRCRAFT WITH SUCH FUSELAGE

    FRANTSISKUS MAJER / KRISTOF MEJSNER / PETER SHTARKE | Europäisches Patentamt | 2015

    Freier Zugriff