Simple and accurate calculations are made of the flow process in a continuous compressorless Lorin jet-propulsion unit. Experimental confirmation is given from towing tests on an airplane at flying speeds up to 200 miles per second. An analysis is made of the performance of a fighter-type airplane designed for utilization of this propulsion system.


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    Title :

    A Ram-Jet Engine for Fighters


    Contributors:
    Sanger, E (author) / Bredt, I (author)

    Publication date :

    1947-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English



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