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Measurements of the velocity field of a hypersonic flow by a laser Doppler velocimeter

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Abstract

An experimental apparatus is described for measuring the local velocities of gas flows in the range from 100 to 10,000 m/sec by means of the Doppler effect. The results of investigations of a free flow and of the same flow over a sphere in a hypersonic wind tunnel at M = 5 are cited and are compared with measurements of velocity using temperature and pressure probes and with theoretical calculations. The behavior of light scattering-particles in the flow is also investigated.

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Literature cited

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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 69–73, July–August, 1974.

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Rinkevichyus, B.S., Tolkachev, A.V. & Kharchenko, V.N. Measurements of the velocity field of a hypersonic flow by a laser Doppler velocimeter. Fluid Dyn 9, 559–562 (1974). https://doi.org/10.1007/BF01031313

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  • DOI: https://doi.org/10.1007/BF01031313

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