Laboratories

Wing profile ( SG1217 , SG1220 )

Favorable pressure gradient boundary layer ( SG2214 , SG1215 )

Flat plate boundary layer ( SG1217 , SG1220 )

Turbulent cylinder wake ( SG2218 , SG3112 )

Heat (Stirling) engine ( SG1216 )

TS-waves ( SG3112 , SG2221 )

Shock tube ( SG2215 )

Biconvex wing profile in compressible flow ( SG2215 )

Compressible pipe flow ( SG2215 )

Drag measurements through wake analysis ( SG3128 , SG2211 )

Wind energy aerodynamics ( SG2226 )

Page responsible:Ramis Örlü
Belongs to: Fluid Physics Laboratory
Last changed: Nov 12, 2014