Articles of The Transactions of KSRC

Full text article (in russian)

Year	2016
Issue	375
Volume	1
Pages	119-124
Caption	Aeroelastic response of anisotropic composite wing subject to turbulent flow effects
Authors	Ya.М. Lybomirov
Keywords	composite polymer materials, cantilever wing, aeroelasticity, self-sustained vibrations, vibration acceleration power spectra
Summary	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.
Rubrics	Naval architecture