A four-year simulation program to develop airworthiness criteria for powered-lift aircraft is summarized. All flight phases affected by use of powered lift (approach, landing, takeoff) are treated with regard to airworthiness problem areas (limiting flight conditions and safety margins: stability, control, and performance; and systems failure). The general features of powered-lift aircraft are compared to conventional aircraft.


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    Titel :

    Airworthiness criteria development for powered-lift aircraft: A program summary


    Beteiligte:
    Heffley, R. K. (Autor:in) / Stapleford, R. L. (Autor:in) / Rumold, R. C. (Autor:in)

    Erscheinungsdatum :

    1977-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airworthiness criteria development for powered-lift aircraft : a program summary

    Heffley, Robert K. / Stapleford, Robert L. / Rumold, Robert C. | TIBKAT | 1977


    Progress Toward Development of Civil Airworthiness Criteria for Powered-Lift Aircraft

    B. C. Scott / C. S. Hynes / P. W. Martin et al. | NTIS | 1976


    Airworthiness Objectives for Civil Powered Lift Aircraft

    Meiklem, P. | Emerald Group Publishing | 1969