Cockpit design of modern highspeed aircraft has become greatly complicated by the need for providing sufficient visual field coverage for the pilot during take-off and landing. This paper is concerned with the problem of specifying minimum required down angles for forward and side vision from the cockpit. A method based on theoretical assumptions is presented, and includes a formula that considers the various factors involved.


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    Titel :

    Cockpit Landing Visibility


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    SAE World Congress & Exhibition ; 1964



    Erscheinungsdatum :

    01.01.1964




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Cockpit landing visibility

    Conover, D.W. | Engineering Index Backfile | 1964


    See and Avoid/Cockpit Visibility

    W. Graham | NTIS | 1989