Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1990-12-03
1991-12-10
Woodiel, Donald O.
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
116201, 116207, G01M 900
Patent
active
050707299
ABSTRACT:
A method is provided for visualizing aerodynamic flow effects on a test surface. First, discrete quantities of a sublimating chemical such as naphthalene are distinctively colored via appropriate dyes or paints. Next, a uniform layer of the sublimating chemical having a particular color is applied to the test surface. This layer is covered with a second uniform layer of a different colored sublimating chemical, and so on until a composite of multi-colored layers is formed having a discrete thickness. Friction caused by an airflow results in the distinctly colored layers being removed in proportion to such aerodynamic flow characteristics as velocity and temperature, resulting in a multi-colored portrait which approximates the airflow on the underlying test surface.
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Osborne Kevin B.
The United States of America as represented by the Administrator
Woodiel Donald O.
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