Infrared technique for aerodynamic flow visualization

Measuring and testing – Wind tunnel: aerodynamic wing and propeller study

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178DIG1, 178DIG8, 250330, G01M 900

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039772446

ABSTRACT:
A method and apparatus for fluid flow visualization of the fluid stream about a model in a fluid circulating facility. An infrared camera is directed at a model through a window in the facility and due to the temperature differential between the model and the fluid, displays the freestream around the model.

REFERENCES:
patent: 2152317 (1939-03-01), Kraner
patent: 2362235 (1944-11-01), Barnes
patent: 2434029 (1948-01-01), Williams
patent: 3325777 (1967-06-01), Fyler
patent: 3566669 (1971-03-01), Lawrence et al.
patent: 3869909 (1975-03-01), Hale et al.

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