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Shear-Sensitive Liquid Crystal Coating Method: Surface-Inclination Effects on Shear Vector MeasurementsThe shear-sensitive liquid crystal coating (SSLCC) method is an image-based technique for both visualizing dynamic surface-flow phenomena, such as transition and separation, and for measuring the continuous shear-stress vector distribution acting on an aerodynamic surface. Under proper lighting and viewing conditions (discussed below), the coating changes color in response to an applied aerodynamic shear. This color-change response is continuous and reversible, with a response time of milliseconds, and is a function of both the shear magnitude and the shear vector orientation relative to the observer. The liquid crystal phase of matter is a weakly-ordered, viscous, non-Newtonian fluid state that exists between the nonuniform liquid phase and the ordered solid phase of certain organic compounds. Cholesteric liquid crystal compounds possess a helical molecular arrangement that selectively scatters white light, incident along the helical axis, as a three-dimensional spectrum. This property is linked to the helical pitch length, which is within the range of wavelengths in the visible spectrum. The pitch length, and hence the wavelength of the scattered light, is influenced by shear stress normal to the helical axis. This unique optical property produces a measurable color change in response to an applied shearing force. The full-surface shear stress vector measurement method, developed at NASA-Ames, is schematically illustrated. As with the visualization method, the coated test surface is illuminated from the normal direction with white light and the camera is positioned at an above-plane view angle of approximately 30 deg. Experiments have been initiated at NASA Ames to begin the process of quantifying surface-inclination (surface-curvature) effects on shear vector measurement accuracy. In preliminary experiments, surface-inclination angles theta(sub x), theta(sub y) of 0, +/-5, +/-10, and +/-15 deg were employed. In this arrangement, white-light illumination was positioned normal to the untilted test surface, and the camera above-plane view angle was set at 30 deg relative to the untilted test surface. As can be seen, vector-aligned lambda(sub d) values showed no dependence on theta(sub x) or theta(sub y) for absolute values of these tilt angles is less than or equal to 15 deg. Acquisition and analyses of full-surface color images are presently underway to definitively document the insensitivity limits of the shear vector measurement methodology to surface-slope variations.
Document ID
20020070795
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Reda, Daniel C.
(NASA Ames Research Center Moffett Field, CA United States)
Wilder, Michael C.
(MCAT Inst. United States)
Nixon, David
Date Acquired
September 7, 2013
Publication Date
November 1, 1998
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 18th International Congress on Instrumentation in Aerospace Simulation Facilities
Location: Toulouse
Country: France
Start Date: June 21, 1999
End Date: June 24, 1999
Sponsors: Office National d'Etudes et de Recherches Aerospatiales
Funding Number(s)
CONTRACT_GRANT: NAS2-14109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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