Effects of turbojet engine unstart on engine operation and characteristics of stall propagation through compressor and inlet system


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    Title :

    Unstart and stall interactions between a turbojet engine and an axisymmetric inlet with 60-percent internal-area contraction


    Contributors:

    Publication date :

    1971-03-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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