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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    Title :

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


    Contributors:

    Conference:

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


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






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