This work offers an approach to analyze the fatigue performance of landing gear of light (single-engine general aviation) aircraft when landing, taking off, or taxiing. Randomness in various properties is taken into account in addition to the random surface profile. The system is modeled as a linear, single degree of freedom, nonstationary vibrating system with random loading and random, time-varying properties; this type of vibration is sometimes referred to as random parametric vibration. This problem is difficult to solve using conventional techniques. The recently-developed random matrix method, which uses the Neumann expansion to obtain statistics of the inverse of a random matrix in terms of the statistics of the elements in the original matrix, is a good technique to use for this problem. Other details of the proposed technique are presented.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Random parametric vibration in aircraft landing gear


    Additional title:

    Regellose, parametrische Schwingung in Flugzeugfahrwerken


    Contributors:


    Publication date :

    1996


    Size :

    6 Seiten, 1 Bild, 15 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Random Parametric Vibration in Aircraft Landing Gear

    Huntington, D. / Lyrintzis, C. / AIAA et al. | British Library Conference Proceedings | 1996




    Random vibration in aircraft landing gear

    Huntington, D. / Lyrintzis, C. | AIAA | 1996


    Landing gear of aircraft and aircraft comprising landing gear

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2021

    Free access