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23 23y
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