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Title: Liquid crystal coatings for surface shear stress visualization in hypersonic flows

Conference ·
DOI:https://doi.org/10.2514/6.1990-1513· OSTI ID:6975863

Experiments were conducted to test the surface-shear-stress visualization capabilities of shear-stress-sensitive/temperature- insensitive liquid crystal compounds in hypersonic flow. Liquid crystal coatings were applied to the surface of a conical model, which was then exposed to a high-unit-Reynolds-number (2.3 {times} 10{sup 7}/m) Mach 5 flow. The coating was illuminated by white light, and its response to the various flow situations was monitored and recorded with standard video and high-speed movie cameras. Boundary layer transition to turbulence was clearly demarcated by the technique. The dynamic location of the transition front as a function of model angle of attack (for sharp and blunt cones, with and without boundary-layer trips) was recorded, and observations were found to be consistent with established (published) trends for hypersonic flows over conical bodies. Normal shock passage over the model during tunnel shutdown was recorded (at 400 frames/second), and the liquid crystal coating was observed to respond to this event in a time interval less than or equal to the time between sequential movie frame exposures ({le} 0.0025 seconds). The liquid crystal technique has thus been demonstrated as a viable diagnostic tool for use in transient/compressible flows. 18 refs., 3 figs.

Research Organization:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Organization:
DOE/DP
DOE Contract Number:
AC04-76DP00789
OSTI ID:
6975863
Report Number(s):
SAND-89-2389C; CONF-9006153-1; ON: DE90010846
Resource Relation:
Conference: 21. AIAA fluid dynamics, plasmadynamics and laser conference in conjuction with the AIAA 25th thermophysics and heat transfer conference and the 16th aerodynamic ground testing conference, Seattle, WA (USA), 18-20 Jun 1990
Country of Publication:
United States
Language:
English