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    Title :

    The Effects of Fixed Conical Spike Inlets on the Performance of Higher Bypass Ratio Engines (AIAA 2018-3836)


    Contributors:

    Conference:

    Aviation technology, integration and operations (Conference)



    Publication date :

    2018-01-01


    Size :

    39 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Nr. 3836

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