The paper discusses the results of selected fatigue tests of a motor glider’s insulated spar structure. The results of the experimental tests were used to assess the potential of the strain-gauge method for diagnosing the spar damage involving the unbolting of one of metal fittings in the spar pin. The usefulness of the deformation measurement method in the composite structure diagnostic process was confirmed, while simultaneously drawing attention to the need for conducting a process optimizing the number of sensors and their distribution on a tested object, in the context of the sensitivity of diagnostic signals received.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Evaluation of the Suitability of the Strain-Gauge Method for Measuring Deformations during the Fatigue Tests of Aviation Composite Structures


    Beteiligte:


    Erscheinungsdatum :

    2017




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    MULTI-COMPONENT STRAIN GAUGE AERODYNAMICS BALANCES IN INSTITUTE OF AVIATION

    Kozniewski, J. / Laskowski, A. / Kania, W. et al. | British Library Conference Proceedings | 2001


    MULTI-COMPONENT STRAIN GAUGE AERODYNAMICS BALANCES IN INSTITUTE OF AVIATION

    Kozniewski, J. / Laskowski, A. / Kania, W. | British Library Online Contents | 2001


    STRAIN GAUGES FOR MEASURING DEFORMATIONS IN MINE OPENING ELEMENTS

    A. E. Pushkarev / F. V. Molev / N. E. Manvelova | DOAJ | 2017

    Freier Zugriff

    Evaluation of Aviation Maintenance Fatigue Countermeasures Training

    O.J Banks / M.B Wenzel / E.K Avers et al. | NTIS | 2013