Aero Lab1 Session2
description
Transcript of Aero Lab1 Session2
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SmokeTunnel,Wakeaftertheairfoil
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Oil filOilfilmflowovertheuppersurfaceofadamagedairfoil
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Flow over a cylinderFlowoveracylinderAluminumpowderinwater
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Flowoveraspheremagnetismfieldg f
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Laminarboundarylayerprofileelectric currentelectriccurrentcausesbubblesmovinginwater
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Global separation on a flat plateGlobalseparationonaflatplateairbubblesinwater
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Flow over cylinderFlowovercylindervisualizationbyairbubblesinwater
Re=2000 Re=10000
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Flow over a slender bodyFlowoveraslenderbodysmokeinjectedfromthebody
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Delta wingDeltawingsmokeinjection
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Slightly supersonic shock waves areSlightlysupersonicshockwavesaremadevisiblebyschilirian cameraM=1.015
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Shock waves over a missileShockwavesoveramissileM=1.1
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Flowoveraspherem=1.5