A diamond-wing configuration has been developed to isolate and study blunt-leading edge vortex separation with both computations and experiments. The wing has been designed so that the results are relevant to a more complex Uninhabited Combat Air Vehicle concept known as SACCON. The numerical and theoretical development process for this diamond wing is presented, including a view toward planned wind tunnel experiments. This work was conducted under the NATO Science and Technology Organization, Applied Vehicle Technology panel. All information is in the public domain.


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    Titel :

    Numerical and Theoretical Considerations for the Design of the AVT-183 Diamond-Wing Experimental Investigations


    Beteiligte:

    Kongress:

    AIAA 2015 SciTech ; 2015 ; Kissimmee, FL, United States
    AIAA Aerospace Sciences Conference ; 2015 ; Kissimee, FL, United States


    Erscheinungsdatum :

    2015-01-05


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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