Limits of engine output; highaltitude engines; influence of air density on proportions of mixture; methods of varying proportions of mixture; automatic prevention of fuel waste; design and application of air-pressure regulators to high-altitude flying. Translated from Technische Berichte, vol. 3, no. 4. (on supp. plates.)


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    Title :

    Adaptation of aeronautical engines to high altitude flying


    Additional title:

    U. S. Nat. Advisory Committee Aeronautics, Technical Notes


    Contributors:


    Publication date :

    1923


    Size :

    30 pages


    Remarks:

    43 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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