The response of an aircraft as a function of time on encountering an isolated ramp gust is derived from its response to a unit step gust. Two Fortran programs are described which treat separately straight ramp and smooth ramp (one-minus-cosine) gust profiles. The (critical) gust length causing maximum dynamic response is determined and responses to simple gust patterns (pairs) are investigated. (Author)


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    Titel :

    The Response of Aircraft to Discrete Ramp Gusts


    Beteiligte:
    A. G. Purcell (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    32 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Houbolt, J.C. | Engineering Index Backfile | 1950


    Recurrence matrix solution for dynamic response of aircraft in gusts

    Houbolt, J.C. | Engineering Index Backfile | 1951


    Recurrence matrix solution for dynamic response of aircraft in gusts

    Houbolt, J.C. | Engineering Index Backfile | 1950