The utilization of image acquisition, image processing and skin friction computations has been developed to support skin friction measurements at the Ludwieg-tube facility at DLR. Verification of the oil-film-interferometry technique with analytical tests at different flows with given shear stress distributions showed its advantages and handicaps for skin friction measurements in 3D gradient flows. The abilities of the thin oil film technique with its application in a short duration wind tunnel were demonstrated on some examples. The comparison of experimental results obtained by different optical skin friction methods demonstrated good agreement.
Prediction of boundary layer transition is important for the design of hypersonic aircrafts. The stu...
on reverie if necessary and identify by block number) FIELD GROUP SUB-GROUP \Skin friction measureme...
In recent years, the independent measurement of wall shear stress with oil-film or oil-drop interfer...
The utilization of image acquisition, image processing and skin friction computations has been devel...
The utilization of image acquisition, image processing and skin friction computations has been devel...
A low-cost setup for oil-film interferometry with white light was used to determine the flow topolog...
A portable dual-laser-beam interferometer that nonintrusively measures skin friction by monitoring t...
As aircraft are designed to a greater extent on computers, the need for accurate and fast CFD algori...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
A method is described for monitoring the changing thickness of a thin oil film subject to an aerodyn...
An improved system for measuring aerodynamic skin friction which uses a dual-laser-beam oil-film int...
Recent improvements in three techniques for measuring skin friction in two- and three-dimensional tu...
The movement of a thin oil film on the surface of fast-rotating disks or propeller blades is analyz...
The movement of the thin oil film placed on the surface of fast-rotating disks or propeller blades i...
The NASA Grant NAG2-261 was initiated to support a program of research to study complex flows that o...
Prediction of boundary layer transition is important for the design of hypersonic aircrafts. The stu...
on reverie if necessary and identify by block number) FIELD GROUP SUB-GROUP \Skin friction measureme...
In recent years, the independent measurement of wall shear stress with oil-film or oil-drop interfer...
The utilization of image acquisition, image processing and skin friction computations has been devel...
The utilization of image acquisition, image processing and skin friction computations has been devel...
A low-cost setup for oil-film interferometry with white light was used to determine the flow topolog...
A portable dual-laser-beam interferometer that nonintrusively measures skin friction by monitoring t...
As aircraft are designed to a greater extent on computers, the need for accurate and fast CFD algori...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
A method is described for monitoring the changing thickness of a thin oil film subject to an aerodyn...
An improved system for measuring aerodynamic skin friction which uses a dual-laser-beam oil-film int...
Recent improvements in three techniques for measuring skin friction in two- and three-dimensional tu...
The movement of a thin oil film on the surface of fast-rotating disks or propeller blades is analyz...
The movement of the thin oil film placed on the surface of fast-rotating disks or propeller blades i...
The NASA Grant NAG2-261 was initiated to support a program of research to study complex flows that o...
Prediction of boundary layer transition is important for the design of hypersonic aircrafts. The stu...
on reverie if necessary and identify by block number) FIELD GROUP SUB-GROUP \Skin friction measureme...
In recent years, the independent measurement of wall shear stress with oil-film or oil-drop interfer...