Problem considered from point of view of balance that must exist between potential and kinetic energy change of aircraft, energy dissipated against drag, and energy derived from fuel; application of energy approach to problems of climb and range; analytical expression relating change in flight altitude to change in gross weight.


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    Title :

    Energy approach to general aircraft performance problem


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1954


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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