The influence of a highly integrated flow-through intake on the vortical flow about a generic lambda wing configuration is studied for 0.55·106


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    Title :

    Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes


    Contributors:

    Published in:

    Publication date :

    2015




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 55.50
    Local classification TIB:    770/7040