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Active control of the wake behind the cylinder
Broučková, Zuzana ; Flídr, Erik ; Šafařík, P. ; Trávníček, Zdeněk
Active control of the flow around a cylinder using synthetic jet (SJ) array was experimentally investigated. The prevailing method was flow visualization. Modification of the wake was investigated at two values of a dimensionless momentum coefficient (Cμ = 0.21 and 1.02). Various α and Cf parameters were tested (where α is the angle between SJs and the main flow direction and Cf is the frequency ratio). The control moves separation point more downstream. Increasing frequency ratio Cf causes refining of the vortex structure. When SJs are placed at the front or rear stagnation points, wake tends towards the symmetrical pattern.
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Small wind tunnel for flow field visualization
Flídr, Erik ; Broučková, Zuzana ; Pavelka, Miroslav ; Trávníček, Zdeněk
This experimental work describes a small wind tunnel for flow field visualization and quantifies its main parameters. Velocity of fluid flow was evaluated by a few experimental methods: - Hot wire anemometry - Videorecord of flow - Velocity measurement at the outlet of the tunnel by hot wire anemometry - Velocity measurement at the outlet of the tunnel by Pitot tube - Continuous velocity measurement at the outlet of the tunnel using the reference Pitot tube Visualization of homogeneous flow field around a circular cylinder was shown.
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Small wind tunnel
Flídr, E. ; Šafařík, P. ; Trávníček, Zdeněk ; Broučková, Z.
The aim of this paper was to describe a small wind tunnel for flow field visualization. Flow velocity was investigated by four methods: hot wire anemometry, Prandtl tube, Pitot tube and flow field visualization were used. Flow pas circular cylinder in Von Kármán regime was shown.
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Measurement of velocity and frequency in synthetic jet
Flídr, E. ; Šafařík, P. ; Trávníček, Zdeněk ; Broučková, Z.
The aim of this paper is to evaluate resonance frequency of pulsation in synthetic jets of air. Resonance frequency was determined by theoretical calculation. This frequency was compared with experimental results. To obtain frequency characteristics three experimental methods were used. Velocity was measured by Pitot tube and hot wire anemometry in CTA regime. Last method was based on calculation of reaction force from relative weight changes.
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