A new optical instrument has been developed for direct measurement of instantaneous velocity gradients at the bounding wall. Light emerging from two tiny optical slits in the surface is used to form a "fan of fringes" in the region very near the wall. Doppler frequency of the light scattered by the
Holographic sensor for measurement of wall velocity gradients
β Scribed by J. E. Millerd; J. P. Swienton; F. Unterscher; J. D. Trolinger; L. G. Smith; J. C. LaRue
- Publisher
- Springer
- Year
- 1996
- Tongue
- English
- Weight
- 861 KB
- Volume
- 21
- Category
- Article
- ISSN
- 0723-4864
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β¦ Synopsis
Time-resolved measurements of skin friction and boundary layer turbulence are important to the design of more fuel efficient aircraft. In this paper we describe the design and testing of a holographic fan fringe sensor that can non-intrusively measure time-resolved velocity gradients near an aerodynamic surface. The holographic sensor produces a set of optical interference fringes inside the viscous sub-layer that form a fan rather than a linear array. Particles scattering light in the sub-layer produce a Doppler frequency that is a direct measurement of the velocity gradient and is proportional to aerodynamic shear stress and skin friction. The holographic recording condenses the optics necessary to form the fringes into a small 3-5 mm package, eliminates the need for optical access from behind the model, and produces a compact and robust sensor.
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