A code-to-code comparison has been performed for high-fidelity simulations ofNASA’s six-passenger quadrotor air taxi con- cept vehicle. Themultidisciplinary simulations combine comprehensive rotorcraft dynamics with high-fidelity fluid dynamics obtained from an unsteady Navier-Stokes computational fluid dynamics code. The results are then compared with those in the literature. A quantitative comparison of converged trim angles has been performed and normal force, chord force, and pitching-moment coefficients arepresented for qualitativecomparison.


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    Titel :

    High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept


    Beteiligte:
    Cameron T Druyor Jr (Autor:in) / Li Wang (Autor:in)

    Kongress:

    Vertical Flight Society Forum 78 ; 2022 ; Fort Worth, TX, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept

    Druyor, C. / Wang | British Library Conference Proceedings | 2022


    COMPUTATIONAL STUDY OF NASA'S QUADROTOR URBAN AIR TAXI CONCEPT

    Diaz, Patricia Ventura / Yoon, Steven | TIBKAT | 2020


    Computational Study of NASA's Quadrotor Urban Air Taxi Concept

    Ventura Diaz, Patricia / Yoon, Steven | AIAA | 2020