The goal of the NASA X-57 Electric Airplane was to utilize the versatility and efficiency of electric propulsion to design a cruise optimized airplane. The wing planform was reduced 42%. A slotted flap and distributed fan system were developed to achieve CL?s in excess of 4.0. Performance objectives, features of the wing and high-lift system, as well as integration considerations will be discussed. CFD performance analysis and details of the integrated structure will be discussed.


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    Titel :

    Inside NASA’s X-57 Configuration - More than Just Electrifying an Airplane


    Beteiligte:
    Jeff Viken (Autor:in)

    Kongress:

    EAA AirVenture ; 2004 ; Oshkosh, WI, US


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :