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Method for laminar boundary layer transition visualization in flight

Assignee: GOVERNMENT OF UNITED STATES NATONAL AERONAUTICS AND SPACE ADMINISTRATION, Administrator of
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Filing: 1986-11-13
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Granted: 1988-10-04
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Expires: 2006-11-13
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Abstract

Abstract Disclosed is a method of visualizing laminar to turbulent boundary layer transition, shock location, and laminar separation bubbles around a test surface. A liquid crystal coating is formulated using an unencapsulated liquid crystal operable in a temperature bandwidth compatible with the temperature environment around the test surface. The liquid crystal coating is applied to the test surface, which is preferably pre-treated by painting with a flat black paint to achieve a deep matte coating, after which the surface is subjected to a liquid or gas flow. Color change in the liquid crystal coating is produced in response to differences in relative shear stress within the boundary layer around the test surface.

Inventors

  • 👤 Bruce J. Holmes
  • 👤 Peter D. Gall

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 22:41
CPC Classifications
G; G01; G01M; G01M9/00; G01M9/06; G01M9/065; G01M9/067; Y; Y10; Y10S; Y10S116/00; Y10S116/43

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 93 words
A method of visualizing laminar to turbulent boundary layer transition, shock location, and laminar separation bubbles around a test surface, the method comprising: formulating a chiral nematic liquid crystal coating using an encapsulated liquid crystal operable in a temperature bandwidth compatible with the temperature environment around the test surface; applying said chiral nematic liquid crystal coating to the test surface; and subjecting the test surface to a liquid or gas flow; whereby a color change is produced in response to differences in relative shear stress within the boundary layer around the test surface.
Claim 2
Independent Claim 93 words
A method of visualizing laminar to turbulent boundary layer transition, shock location, and laminar separation bubbles around a test surface, the method comprising: formulating a chiral nematic liquid crystal coating using an encapsulated liquid crystal operable in a temperature bandwidth compatible with the temperature environment around the test surface; applying said chiral nematic liquid crystal coating to the test surface; and subjecting the test surface to a liquid or gas flow; whereby a color change is produced in response to differences in relative shear stress within the boundary layer around the test surface.
Claim 3
Dependent Claim 36 words
A method according to claim 1 wherein the test surface is prepared by painting with a flat, black paint to achieve a deep matte coating which is capable of absorbing the chiral nematic liquid crystal material.

References Cited (Backward Citations)

US3529156A Cited
US3511086A Cited
US3620889A Cited
US3787874A Cited
US3847139A Cited
US4101696A Cited
US4175543A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-10-04 1992-04-04 1992-10-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-10-04 1996-04-04 1996-10-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-10-04 2000-04-04 2000-10-04 $7700.00 Window Closed / Lapsed

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