The present study proposes a pseudorotation adjoint-based aerodynamic and aeroacoustic optimization method for the application on isolated rotors with both accuracy and efficiency. The pseudorotation adjoint-based optimization methodology incorporates two innovative techniques: i) a hybrid computational fluid dynamics–computational aeroacoustics method closely integrating with Reynolds-averaged Navier–Stokes equations under a rotating reference frame within a pseudorotation moving-medium Ffowcs Williams-Hawkings formulation to evaluate aerodynamic performance and tonal noise, and ii) a unified architecture for steady-state adjoint-based sensitivity analyses of both aerodynamics and aeroacoustics leveraging the pseudorotation approach, thereby facilitating effective multi-objective weighted optimizations within one comprehensive framework. The proposed pseudorotation steady adjoint-based optimization method is applied to a bidiscipline optimization problem of rotor blades compared with our previous on-the-fly unsteady adjoint method. Results of the comparative study demonstrate that the pseudorotation steady approach exhibits good agreement with the unsteady approach in predicting aerodynamics and aeroacoustics as well as their sensitivity derivatives. Furthermore, the steady adjoint optimization demonstrates its capability in achieving an optimum rotor design that closely resembles the outcome from unsteady adjoint optimization while exhibiting a 20-fold acceleration in computational time. These results highlight the potential of this proposed pseudorotation adjoint-based optimization method in efficiently exploring fundamental principles governing high aerodynamic performance and low tonal noise emissions for isolated rotors.
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