THE values of the load factors used in de-signing an aeroplane are almost direct measures of its strength. They also affect the weight of a certain portion of the aeroplane structure. Although the percentage of gross weight that depends directly on the magnitude of the design load factors is not as large as might be supposed, it represents a considerable potential pay load on large aeroplanes and therefore warrants careful consideration of the basic question: What is the minimum load factor consistent with safety?


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    Titel :

    Flight Load Factors


    Untertitel :

    The First of Two U.S. Civil Aeronautics Authority Reports for the Information of Pilots


    Erschienen in:

    Erscheinungsdatum :

    01.03.1941


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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