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Determination of the shape of the shocks ahead of a transverse jet injected into a supersonic flow

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Abstract

The three-dimensional shape of the shock wave formed ahead of a sonic jet flowing out into a supersonic flow through the surface of a sharp cone is determined. The shape of the wave in the longitudinal and transverse cross-sections of the model is constructed using schlieren photographs taken for various angles of rotation and freestream Mach numbers M=1.75–3.

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References

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Authors
  1. M. D. Anokhin
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  2. Yu. A. Vinogradov
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  3. A. I. Zubkov
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  4. B. E. Lyagushin
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  5. Yu. A. Panov
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Additional information

Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 2, pp. 41–44, March–April, 1998.

This research was carried out with financial support from the Russian Foundation for Basic Research (project No. 95-01-00709a).

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Anokhin, M.D., Vinogradov, Y.A., Zubkov, A.I. et al. Determination of the shape of the shocks ahead of a transverse jet injected into a supersonic flow. Fluid Dyn 33, 186–189 (1998). https://doi.org/10.1007/BF02698700

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  • DOI: https://doi.org/10.1007/BF02698700

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