Keywordsaerodynamic noise; NLAS; kriging model; cross validation; equivalent continuous SPL; structural acoustics; vibroacoustic; uncertainty quantification; reduced-order model; medium frequency; low frequency; dissipative system; wall acoustic impedance; finite element discretization; boundary element method; vibration analysis; acoustic analysis; FEM; BEM; NVH; modal analysis; jet-noise; stochastic noise generation and radiation; Reynolds Averaged Navier Stokes; Large Eddy Simulations; cavity tone; direct aeroacoustic simulation; aeroacoustics; plasma actuators; flow control; noise control; vortices; wind tunnel experiments; acoustic sources; Computational Fluid Dynamics (CFD); helicopter main rotor; tail-boom vibration; Euler-Bernoulli equation; aeroacoustics; flow-excited; vibration; sound radiation; acoustic coupling; turbulent; boundary layer; aerodynamic noise; valve noise; pipe flow; wavenumber-frequency analysis; transport; noise; acoustics; rocket; analysis; n/a; neural network; system identification; nonlinear aeroelastic
