Wall shear stress and wall streamline direction measurements were conducted on a generic delta wing model to demonstrate the potential of the white-light oil-film interferometry in three-dimensional flows. With the proposed algorithm, an automatic oil-film thickness calculation is possible and yields reproducible and plausible wall shear stress distributions on the leeward side of the delta wing for various angles of attack
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...
The NASA Grant NAG2-261 was initiated to support a program of research to study complex flows that o...
Wall shear stress and wall streamline direction measurements were conducted on a generic delta wing ...
A low-cost setup for oil-film interferometry with white light was used to determine the flow topolog...
A simple setup for oil-film interferometry with white light was used to determine the flow topology ...
There is continuing debate regarding the validity of skin friction measurements that are dependent o...
In recent years, the independent measurement of wall shear stress with oil-film or oil-drop interfer...
Wall shear stress is an important parameter in accessing the aerodynamics performance of an object. ...
A method is described for monitoring the changing thickness of a thin oil film subject to an aerodyn...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
Turbulent boundary layer flow research uses oil film and oil drop interferometry to measure wall she...
In wall-bounded turbulent flows, determination of the wall shear stress is an important task. A prim...
The absence of a model to predict near wall viscosity of complex suspensions instigated an investiga...
A portable dual-laser-beam interferometer that nonintrusively measures skin friction by monitoring t...
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...
The NASA Grant NAG2-261 was initiated to support a program of research to study complex flows that o...
Wall shear stress and wall streamline direction measurements were conducted on a generic delta wing ...
A low-cost setup for oil-film interferometry with white light was used to determine the flow topolog...
A simple setup for oil-film interferometry with white light was used to determine the flow topology ...
There is continuing debate regarding the validity of skin friction measurements that are dependent o...
In recent years, the independent measurement of wall shear stress with oil-film or oil-drop interfer...
Wall shear stress is an important parameter in accessing the aerodynamics performance of an object. ...
A method is described for monitoring the changing thickness of a thin oil film subject to an aerodyn...
Accurate skin friction measurements are indispensable in the design of more efficient aerodynamic ve...
Turbulent boundary layer flow research uses oil film and oil drop interferometry to measure wall she...
In wall-bounded turbulent flows, determination of the wall shear stress is an important task. A prim...
The absence of a model to predict near wall viscosity of complex suspensions instigated an investiga...
A portable dual-laser-beam interferometer that nonintrusively measures skin friction by monitoring t...
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...
The NASA Grant NAG2-261 was initiated to support a program of research to study complex flows that o...