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Numerical simulation and experiments with the profile NACA 0012
Chládek, Štěpán ; Zolotarev, Igor ; Uruba, Václav
This paper introduces the new model of the airfoil and describes both aeroelastic experiments and numerical simulation with the profile NACA 0012. The aeroelastic is the science which studies the flow-structure interaction. The flow field can cause change of the position of the solid body and the body due to the change of its position influences the flow field. Mathematical description of the interaction has to involve both the equations of the fluid dynamic and the equations of motion of the solid body. The first results will be presented from the measuring in the dynamic laboratory and from the measuring in the wind tunnel. The main aim of the experimental part of this research is to cause a self-oscillated motion of the airfoil and to measure the transient flow field during this motion. The numerical part should be identical with the experimental dates.
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The self-excited vibration of the NACA0015 profile
Vlček, Václav ; Zolotarev, Igor ; Kozánek, Jan
The two-dimensional flow patterns around the profile NACA0015 vibrating in self-excitation modes were measured in the wind tunnel by optical methods. The Mach numbers for the self-excited vibrations were in the interval 0.2 – 0.45. Results of the interferometric measurement and the profile kinematic movements during the self-oscillations are presented.
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Interaction and Feedbacks 2011
Zolotarev, Igor
Proceedings INTERACTION AND FEEDBACKS 2011 deals with the problems of interactions of dynamic systems with surrounding liquid or fluent environment and the solutions of the dynamic systems with feedbacks.
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The self-excited vibration of the isolated profile in wide interval of Mach numbers
Vlček, Václav ; Kozánek, Jan ; Zolotarev, Igor
In this paper the experimental results of the self-excited vibration of the isolated NACA0015 profile in subsonic airflow are given. The optical and pneumatical methods were used in the wide range of flow velocities (Mach numbers 0,18 – 0,45). The profile was equipped with semi-conductor pressure sensors situated in the profile surface. From obtained interferograms and pressure signals follow complicated relation among phase differences of rotational and transversal profile movement.
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Forces actingon the fluttering. Profile in the wind tunnel
Vlček, Václav ; Kozánek, Jan ; Zolotarev, Igor
2D experiments with profile NACA0015 supported with two degrees of freedom in aerodynamic tunnel of suction type were realized. One degree of freedom was rotation around the profile axis in 1/3 chord distance behind the profile leading edge, the second one was the vertical translation. The interferometric visualization of the flow field in the vicinity of the profile during its self-excited vibration was realized. Forces acting on the profile and the pressure distribution on the profile surface resulting from the interferometric measurements are presented.
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Mathematical model of the support of experimental aerodynamical profile
Kozánek, Jan ; Bula, Vítězslav ; Zolotarev, Igor
In this paper the simple mathematical model of longitudinal and angular vibrating motion of experimental aerodynamical NACA0015 profile is given. With the help of dynamical experiments from complex frequency responses are by least squares fitting method identified complex eigenvalues. The direct identification method defines real coefficient matrices (of order 2) of stiffness, damping and mass of this non-conservative dynamical system. Finally, the comparisons of measured and from mathematical model evaluated responses are given and discussed.
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Vibrace vyvolané proudem tekutiny 2008
Zolotarev, Igor ; Horáček, Jaromír
Flow-induced vibrations and noise continue to cause problems in a wide range of engineering applications, ranging from mechanical and aerospace engineering, civil engineering and ship and offshore structures to power generation and chemical processing. These proceedings bring together 139 papers dealing with a variety of topics relating to flow-induced vibration and noise, such as:vortex-induced vibration, vibration of heat-exchanger tube bundles,progress in fluid-structure interaction theory and CFD simulations, flow-sound interaction, biomechanics of voice and hearing, thermo-acoustic instabilities, vibration of hydraulic structures, gates, turbomachines nad piping systems. The contents of this publication constitute a „mixture“ of investigations by those working on the mechanisms of vibration and means of their alleviation, and studies by those in industry who draw on the present state of knowledge of these mechanisms to avoid or solve flow induced vibratin and noise problems in industrial and other applications.
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