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.
High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept
Vertical Flight Society Forum 78 ; 2022 ; Fort Worth, TX, US
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aerodynamics , eVTOL , CFD
High-Fidelity Analysis of Six-Passenger Quadrotor Air Taxi Concept
British Library Conference Proceedings | 2022
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