Optimal Reduced Basis Method for Aeroacoustics with Impedance Boundary Conditions - DMPE ONERA
Article Dans Une Revue AIAA Journal Année : 2023

Optimal Reduced Basis Method for Aeroacoustics with Impedance Boundary Conditions

Résumé

Solving the linearized Euler equations in the harmonic frequency domain amounts to solving a large linear system. Doing so repetitively can be costly, especially when some parameters need to be varied (for example, the acoustic impedance of a liner), such as in optimization and impedance eduction problems. To accelerate the calculations, the equations can first be projected onto a basis of reduced dimension, only requiring a limited number of full solutions called snapshots, which are calculated at different impedance values. This paper is concerned with finding an optimal set of impedances allowing the greedy creation of a reduced basis that leads to the most accurate surrogate modeling in the least number of calls to the direct solver. The optimal set of impedance values is first obtained on a two-dimensional duct configuration, and numerical verification tests are performed on a three-dimensional engine nacelle.
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Dates et versions

hal-04748386 , version 1 (25-10-2024)

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Rémi Roncen, Philip Edel, Christophe Peyret. Optimal Reduced Basis Method for Aeroacoustics with Impedance Boundary Conditions. AIAA Journal, 2023, 61 (2), pp.640-652. ⟨10.2514/1.J062138⟩. ⟨hal-04748386⟩
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