When the laminar-to-turbulent transition occurs close to the blade trailing edge, the periodic
passage of shear layer roll-up vortices over the trailing edge would influence the unsteady …

A lattice-Boltzmann method has been employed to study the aeroacoustics and
aerodynamics of airfoils equipped with leading edge treatments, namely the porous leading …

Advanced mesh generation and update methods for parallel 3D computation of complex
flow problems are presented. The complexities of the class of problems targeted include …

A hybrid method is applied to predict trailing edge noise based on a large eddy simulation
(LES) of the compressible flow problem and acoustic perturbation equations (APE) for the …

This study utilizes a hybrid aeroacoustic model to investigate how airfoils with spanwise
wavy geometries can be used to reduce trailing-edge noise alongside improving the …

A numerical method for the prediction of an unsteady fluid flow in a complex geometry that
involves moving boundary interfaces is presented in this paper. The method is also …

The paper applies a wavelet filtering method based on the recursive denoising algorithm to
airfoil noise in low-Mach number flows. The pressure field around the airfoil is decomposed …

Sound generated by an airfoil in the wake of a rod is predicted numerically by using a
Detached-Eddy Simulation (DES) unsteady flow field and a Ffowcs Williams and Hawkings …

A computational methodology is proposed for aerodynamic noise prediction of long-span
bodies at low Mach numbers. The three-dimensional hydrodynamic field is computed by …

ABSTRACT A numerical investigation is conducted on aerodynamic noise of flow past a
circular cylinder with different spanwise lengths (0.5 pD, pD, 2pD, and 4pD) at Re ¼10000 …