Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computational Evaluation of Inlet Distortion on an Ejector Powered Hybrid Wing Body at Takeoff and Landing Conditions (Invited)



    Conference:

    54th AIAA Aerospace Sciences Meeting



    Publication date :

    2016-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English