This article provides information about in-flight measurement of a small sport aircraft. First strain gauges were installed in the wing structure and then calibration procedures were done. After the calculation of strain gauge coefficients, equations for calculating bending moments and other variables were established. A data acquisition system was installed in the aircraft to measure responses from strain gauges and other variables such as speed, altitude, load factor, and temperature. Many flights were performed with the aircraft equipped this way, and after that the recorded data were analysed and those results were compared with the calculations and static strength tests performed before.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Possibilities and methods of in-flight loading measurement


    Beteiligte:
    Ivo Jebáček (Autor:in) / Marek Horak (Autor:in)


    Erscheinungsdatum :

    2012




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Panel Methods in Flight Machanics - Possibilities and Limitations

    Goraj, Z. / Sznajder, J. | British Library Online Contents | 1995


    Possibilities of a trans-pacific flight

    Westervelt, G.C. / Sanford, H.B. | Engineering Index Backfile | 1920


    POSSIBILITIES OF REALLY HIGH-SPEED FLIGHT

    Victory, John F. | SAE Technical Papers | 1946


    Bandwidth Enabled Flight Operations: Examining the Possibilities

    Pisanich, Greg / Renema, Fritz / Clancy, Dan | NTRS | 2002