Note shows that propeller can be designed to give satisfactory aerodynamic characteristics for flight at 50,000 ft, that it will give relatively poor performance at low altitudes, that take-off will be fair, but that weight will be excessive; equations and formulas included.


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    Title :

    Speculations on propellers for stratosphere airplanes


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Ober, S. (author)


    Publication date :

    1937


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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