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Area Measurement of Skin Friction in Complex Three-Dimensional Flows
by Brown, James L
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A surface-imaging skin-friction instrument provides
measurement of the wall shear-stress vector over a large
surface region during a single wind tunnel test using an
oil-film interference method. During a test, a camera
captures images of the fringe pattern produced by
illuminating an oil film with quasi-monochromatic light.
By using a visual tracer in the oil, the surface
streamlines can also be determined. Analysis of the
fringe images using a Hilbert-transform-based technique
determines the oil thickness distribution in the region
where fringes are visible. A combination of the oil
thickness and surface direction is then used to calculate
the surface shear-stress distribution by numerically
solving the thin-oil film equation: where tau(sub x) and
tau(sub z) are the x- and z-components of the surface
shear stress, and mu is the dynamic viscosity of the oil.
All quantities in this equation are known from the height
measurement except tau(sub x) and tau(sub z). However, an
additional piece of information is needed to solve this
equation. If the surface streamline direction gamma is
obtained from visual tracers or from a streamline image,
then tau(sub x) = tau cos(gamma) and tau(sub z) = tau
sin(gamma), and the equation may be solved for tau. To
test the technique in a demanding situation, it was
applied to a three-dimensional (3-D) flow in which a
cylinder is mounted normal to a flat plate. An incoming
turbulent boundary layer encounters the vertically
mounted cylinder and a highly complex 3-D flow results.
Date Published: 2011-06-02 08:33:55
Identifier: nasa_techdoc_20040075818
Item Size: 6602804
Language: eng
Media Type: texts
# Topics
GALILEAN SATELLITES
EUROPA
CRATERING
GANYMEDE
IO
PLANETARY SURFACES
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nasa_techdocs
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