The aeroelastic measurements on the oscillating NACA0015 profile vibrating as the dynamic system with two degrees of freedom (pitch and plunge) were realized within the i [...]

The aeroelastic experiments realized in wind tunnel of the Institute of Thermomechanics with Mach numbers M ~ 0.20-0.22 and with the interval of Reynolds numbers Re = (2. [...]

The paper describes computation of aerodynamic damping and natural frequencies of aeroelastic systems. The damping is a critical parameter for the stability analysis of a [...]

The two-dimensional flow pattern around the vibrating profile NACA0015 with his selfexcitation mode was measured in the wind tunnel by optical methods. The used profile w [...]

This paper introduces the new model of the airfoil and describes both aeroelastic experiments and numerical simulation with the prof le NACA 0012. Mathematical descriptio [...]

Aeroelastic experiments with the profile NACA0015 were realized in the suction type aerodynamic tunnel of the Institute of Thermomechanics, Czech Academy of Sciences, Pra [...]

This paper introduces an identification of an aeroelastic profile as n – degrees of freedom linear system. The common identification is based on the excitation of the s [...]