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Jet flow issuing from an axisymmetric pipe-cavity-orifice nozzle
Broučková, Zuzana ; Pušková, P. ; Trávníček, Zdeněk ; Šafařík, P.
Axisymmetric air jet flow is experimentally investigated under passive flow control. Jet issues from a pipe (inner diameter 10mm, length 150 mm) equipped with an axisymmetric cavity at the end. Cavity operates as resonator creating self-sustained acoustic excitations. Mechanism of excitations is complex. Experimental methods were: flow visualization, microphone measurements and velocity measurements by the Pitot probe. Power spectral density (PSD) and sound pressure level (SPL) were evaluated from microphone measurements. Jet Reynolds number ranged Re = 1600–18 000. Peaks in PSD indicated a function of the resonator. The most effective acoustic response was found at higher Re. Results demonstrate effects of the control: mixing and velocity decay along the axis are intensified. It causes shortening of the transition region. However, an inverse proportionality of the velocity decay in the fully developed region is not changed. Momentum and kinetic energy fluxes decrease more intensively.
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Pasivní řízení symetrického proudu vzduchu
Pušková, P. ; Šafařík, P. ; Trávníček, Zdeněk ; Broučková, Z.
Práce se zabývá pasivním řízením osově symetrického proudu vzduchu pomocí rezonátoru. Cílem je zjistit, jak ovlivňuje rezonátor chování proudu. Pro ověření známých teoretických poznatků je experimentálně naměřena frekvenční charakteristika Helmholtzova rezonátoru. Dále je zjištěna spektrální výkonová hustota signálu z mikrofonu pro jednotlivé režimy proudění (Re = 1600, 5000, 10 000 a 30 000) a různé objemy rezonátoru. U vybraných režimů jsou naměřeny vlastnosti proudu (poklesy rychlosti v ose proudu a rychlostní profily) pomocí Pitotovy sondy. Následně jsou porovnány vlastnosti proudu bez rezonátoru a s rezonátorem.
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Visualisation of Boundary Layer Separation and Passive Flow Control on Airfoils and Bodies in Wind-Tunnel and In-Flight Experiments
Popelka, Lukáš ; Kuklová, J. ; Šimurda, David ; Součková, Natálie ; Matějka, Milan ; Uruba, Václav
Infrared camera, Particle Image Velocimetry, smoke-wire, tuft filaments and oil-flow visualization techniques were used for wind-tunnel and in-flight investigation of boundary layer separation, both stall and separation bubbles, related to the low-Reynolds numbers transition mechanism. Airfoils of Wortmann FX66 series and FX66 series wing-fuselage interaction, as well as modern airfoils and their wing-fuselage geometry were subject to study. The presence of previously identified structures in the CFD modelling, such as horse-shoe vortices, was confirmed in the flow.
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