Lift coefficient for maximum range is graphically and analytically determined; engine overall efficiencies discussed in their relation to range considerations; maximum range expression derived for case of constant altitude and for case of constant engine and air speed, and the two expressions are compared.


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    Title :

    Jet airplane range considerations


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Jonas, J. (author)


    Publication date :

    1947


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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