Measuring and testing – Wind tunnel: aerodynamic wing and propeller study
Patent
1991-08-08
1993-01-12
Raevis, Robert
Measuring and testing
Wind tunnel: aerodynamic wing and propeller study
73 9, G01M 900
Patent
active
051780046
ABSTRACT:
A housing block is provided having an upper surface conforming to the test surface of a model or aircraft. An oil film is supplied upstream of a transparent wedge window located in this upper surface by an oil pump system located external to the housing block. A light source located within the housing block supplies a light beam which passes through this transparent window and is reflected back through the transparent window by the upper surface of the oil film to a photo-sensitive position sensor located within the housing. This position sensor allows the slope history of the oil film caused by an aerodynamic flow to be determined. The skin friction is determined from this slope history. Internally located mirrors augment and sensitize the reflected beam as necessary before reaching the position sensor. In addition, a filter may be provided before this sensor to filter the beam.
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L. H. Tanner, "A skin friction meter, using the viscosity balance principle, suitable for use with flat or curved metal surfaces." J. of Physics E: Scientific Instruments, vol. 10, (printed in Great Britain), 1977, pp. 278-284.
Weinstein, L. M. and Bandyopadhyay, P. R. "A Simplified Oil-Film Skin-Friction Meter", First National Fluid Dynamics Congress, Cincinnati, Ohio, Jul. 25-28, 1988, (AIAA/ASME/SIAM/APS).
Seto, J. and Hornung, H. G., "Internally Mounted Thin-Liquid-Film Skin-Friction Meter--Comparison with Floating Element Method With and Without Pressure Gradient", AIAA 91-0060, CA Institute of Technology, Pasadena, Calif., 29th Aerospace Sciences Meeting, Reno, Nev. Jan. 7-10, 1991.
Bandyopadhyay Promode R.
Weinstein Leonard M.
Osborne Kevin B.
Raevis Robert
The United States of America as represented by the Administrator
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