Formulas for constant altitude range, endurance, and average operating speed derived; charts simplify solution of expressions and are applicable to any turbojet airplane; charts presented for two flight conditions, maximum range flight and flight at constant airspeed, and both conditions are considered for ferry mission and for mission where bombs or cargo are dropped at range midpoint.


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    Title :

    Determination of constant altitude range performance of turbojet-propelled aircraft


    Additional title:

    Ky Univ -- Eng Experiment Station -- Bul


    Contributors:


    Publication date :

    1950


    Size :

    22 pages


    Remarks:

    Charts in pocket


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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