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Numerické simulace interakce neviskozního a viskozního proudění nestlačitelné tekutiny s vibrujícím profilem
Honzátko, R. ; Horáček, Jaromír ; Kozel, Karel
The work deals with a numerical solution of the interaction of 2D incompressible flows and a freely vibrating profile with large amplitudes. The profile can oscillate around an elastic axis and in the vertical direction. The motion of the profile is described by two nonlinear ordinary differential equations solved numerically using four-order Runge-Kutta method. The Euler or Navier-Stokes equations represent the inviscid or viscous flows. Numerical schemes of the finite volume method are applied on a structured quadrilateral C-mesh. The method of artificial compressibility and dual-time stepping method are employed for numerical solution. Deformations of the computational domain due to the profile motion are treated using the ALE method.
Vibrace leteckéhoj profilu se třemi stupni volnosti vybuzené proudem vzduchu
Růžička, M. ; Feistauer, M. ; Horáček, Jaromír ; Sváček, Petr
The subject of this article is the numerical simulation of the interaction of two-dimensional incompressible viscous fluid and a vibrating airfoil with large amplitudes. a solid airfoil with three degrees of freedom can rotate around the elastic axis, oscillate in the vertical direction and its flap can rotate. the numerical simulation consists of the finite element solution of the Navier-Stokes equations coupled with a system of nonlinear ordinary differential equations describing the airfoil motion. The time-dependent computational domain and moving grid are taken into account with the aid of the Arbitrary Lagrangian-eulerian (ALE) formulation. High Reynolds numbers up to 10 6 require the application of a suitable stabilization of the finite element discretization. Numerical tests and comparison with NASTRAN solver prove that the developed method is sufficiently accurate and robust.
Vizualizace nestacionárního proudění kolem vibrujícího profilu
Vlček, Václav ; Horáček, Jaromír ; Luxa, Martin ; Veselý, Jan
The contribution presents results of optical measurements of flow field around a vibrating double circular arc (DCA) 18% profile elastically supported in the measurement section of a wind tunnel. The profile can vibrate with two degrees of freedom for translation and rotation. the schlieren and interferometry methods were used for visualization of a two-dimensional flow in different phase of the profile motion. The measurements were performed in a subsonic wind tunnel above the airflow velocity for loss of the system stability by flutter, thus the vibration amplitudes were relatively large up to about+-4mm for vertical translation and +-6 degrees for angle of rotation around the elastic axis. The images of the flow field were recorded for prescribed phase delays during one oscillation period of the profile from which the pressure and velocity were evaluated in given time instants.
Visualization of unsteady flows around vibrating profile
Vlček, Václav ; Horáček, Jaromír ; Luxa, Martin ; Veselý, Jan ; Vaněk, František ; Bula, Vítězslav ; Vávra, J.
The contribution presents preliminary results of interferometry measurements of flow field around a vibrating double circle 18% profile above the critical airflow velocity for loss of the system stability by flutter. The measurements were performed in subsonic wind tunnel for prescribed phase delays during one oscillation period of the profile with two degrees of freedom for rotation and translation.
Measurement of unsteady flow fields around a vibrating profile by optical methods
Horáček, Jaromír ; Vlček, Václav ; Luxa, Martin ; Veselý, Jan ; Vaněk, František ; Bula, Vítězslav ; Vávra, J.
The report presents preliminary results of interferometry measurements of flow field around a vibrating double circle 18% profile above the critical airflow velocity for loss of the system stability by flutter. The measurements were performed in subsonic wind tunnel for prescribed phase delays during one oscillation period of the profile with two degrees of freedom for rotation and translation.
Natural vibrations and stability of cylindrical shells in interaction with flowing fluid
Horáček, Jaromír ; Zolotarev, Igor
Natural frequencies and thresholds of stability of thin cylindricaal shell conveying or surrounded by flowing fluid are theoretically studied. Viscous fluid forces are modelled by the Darcy law, and effects of fluid compressibility are discussed. Particularly the effects of fluid viscosity and the type of boundary conditions at the edges of the shell on the critical flow velocities are demonstrated.
Dynamic characteristics and stability of cylindrical shell conveying fluid
Horáček, Jaromír ; Dubuc, F.
Natural frequencies and the thresholds for loosing the hydroelastic stability of thin-walled cylindrical shell conveying fluid are theoretically studied. Potential flow theory for fluid and semi-membrane theory for the shell are used. The viscous fluid forces are modelled by the Darcy law. The fundamental importance of boundary conditions considered for fixing the edges of the cylindrical shell of finite length is shown.
Mathematical model of vocal fold vibrationh excited by air-structure interaction-numerical calculations
Horáček, Jaromír ; Švec, J.
Frequency-modal and stability analysis of the developed aeroelastic model of vocal fold vibration in the phonatory airflow are presented. Stability maps calculated for four distinct models with different types of elastic support and aerodynamic vocal
Instability onset of rectangular prismatic beams in the wind flow
Pospíšil, Stanislav ; Fischer, Cyril ; Náprstek, Jiří
This paper describes a part of theoretical and experimental researchdealing with the problem of the aeroelastic instability onset ofslender rectangular beams in the air stream, modeled as twodegrees-of-freedom.
Design of an experimental set up for studies of 2D unsteady aeroelastic phenomena by optical methods
Horáček, Jaromír ; Luxa, Martin ; Vaněk, František ; Veselý, Jan ; Vlček, Václav
The report is an introductory study in the design of optical methods for visualization of unsteady flow fields near a vibrations profile with two degrees of freedom. The report contains description of the aeroelastic model, the results of measurements of dynamic and aeroelastic characteristics of the model in the wind tunnel and design of methodology for the optical measurements including schemes of special synchronization electronic circuits and the overall device connection arrangement.

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