Purpose of study is to show application of perturbation technique in study of random response of multidegree-of-freedom nonlinear system simulating airplane moving with constant velocity along runway whose profile is represented by stationary random process; using pertinent characteristics of supersonic civil transport being designed in United States, numerical results are produced for response of simplified idealization of airplane; applicable to evaluation of fatigue damage of landing gear system and structural damage of airframe due to runway roughness.


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    Titel :

    Effects of runway roughness on dynamic response of airplanes


    Weitere Titelangaben:

    J Sound Vibration


    Beteiligte:
    Tung, C.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Schlagwörter :





    Runway Roughness Criteria

    Filarski, J. D. / American Society of Civil Engineers | British Library Conference Proceedings | 2001


    Runway roughness effects on new aircraft types

    Lee, H.R. / Scheffel, J.L. | Engineering Index Backfile | 1968