Expressions developed for max range for three cruise flight conditions: constant altitude, varying altitude below 35,000 ft, and varying altitude above 35,000 ft; max range obtained by increasing cruising altitude as fuel is consumed; airplane configurations derived which correspond to aerodynamic optima for cruise conditions investigated; importance of thrust loading. (See also - discussion n 6 June p 341-2)


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    Title :

    Range performance of turbojet airplanes


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :