In one embodiment, an aircraft includes a number of propellers Nprop, wherein each propeller comprises a diameter dprop, has a propeller efficiency ηprop, and is configured to absorb power pprop to rotate at a rate RPM to generate thrust for a flight speed V of the aircraft. The aircraft may further include a total power ptotal absorbed by the propellers that is approximately pprop×Nprop, a wing having a circulation distribution, wherein the wing comprises a wingspan B, a drag D that is approximately equal to ptotal×ηprop/V. For V and B, the circulation distribution, dprop, and RPM substantially minimizes D.


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    Titel :

    Wing and Propeller Design for Aircraft


    Beteiligte:
    LIU ZHANG (Autor:in) / TALMOR AMNON G (Autor:in) / CAO YUSONG (Autor:in)

    Erscheinungsdatum :

    2018-10-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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