Main advantage is resultant small weight for given thrust; application of small turbines to aircraft results in increase of payload, speed or range, or compromise between these variables; field of application.


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    Title :

    Case for small turbine engines


    Additional title:

    Can Aeronautical J


    Contributors:
    Eden, J.J. (author)

    Published in:

    Publication date :

    1955


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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