Publication | Closed Access

A WAVENUMBER APPROACH TO MODELLING THE RESPONSE OF A RANDOMLY EXCITED PANEL, PART II: APPLICATION TO AIRCRAFT PANELS EXCITED BY A TURBULENT BOUNDARY LAYER

AeroacousticsEngineeringAerospace EngineeringAerospace SimulationTurbulence ModelingNumerical SimulationAerodynamicsModeling And SimulationTurbulent FlameBoundary LayerPart Ii