Results of analysis illustrated by graphs showing comparative effectiveness of different methods of increasing flying speed; high wing loading presents greatest need for higher speeds at sea level; optimum wing loading for maximum flying speed shown to be that required to fly at maximum L/D of wing and tail surfaces. Before Inst Aeronautical Sciences.


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    Title :

    Some problems in design of high-speed aircraft


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1938


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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