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SmokeTunnel,Wakeaftertheairfoil

Oil filOilfilmflowovertheuppersurfaceofadamagedairfoil

Flow over a cylinderFlowoveracylinderAluminumpowderinwater

Flowoveraspheremagnetismfieldg f

Laminarboundarylayerprofileelectric currentelectriccurrentcausesbubblesmovinginwater

Global separation on a flat plateGlobalseparationonaflatplateairbubblesinwater

Flow over cylinderFlowovercylindervisualizationbyairbubblesinwater

Re=2000 Re=10000

Flow over a slender bodyFlowoveraslenderbodysmokeinjectedfromthebody

Delta wingDeltawingsmokeinjection

Slightly supersonic shock waves areSlightlysupersonicshockwavesaremadevisiblebyschilirian cameraM=1.015

Shock waves over a missileShockwavesoveramissileM=1.1

Flowoveraspherem=1.5