Aeroelastic response of anisotropic composite wing subject to turbulent flow effects
The paper presents results of numerical simulation study on turbulent flow near a thin trailing edge of wing. Aeroelastic response of anisotropic carbon-fiber reinforced composite wing subject to incident incompressible gas flow is analyzed. It is shown that analytical estimates of the wing vibration acceleration power spectra (with wing subject to turbulent velocity fluctuations at trailing edge) agrees well with experimental results.