Study based on fundamental equations of flight and propeller data contained in reports of Nat. Advisory Committee for Aeronautics. It is concluded that under best conditions and assuming that data available could be proportionally reproduced at high altitudes, aeroplane could be designed to give speed of 260 m.p.h. at about 50, 000 ft. altitude.


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    Titel :

    Factors involved in high airplane speed at great altitudes


    Weitere Titelangaben:

    Jl. Soc. Automotive Engrs


    Beteiligte:


    Erscheinungsdatum :

    1920


    Format / Umfang :

    5 pages


    Anmerkungen:

    7 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    FACTORS INVOLVED IN HIGH AIRPLANE SPEED AT GREAT ALTITUDES

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    Kru¨ / ger, R. | Engineering Index Backfile | 1919