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Flow structure formed due to interaction of a supersonic jet with a porous obstacle

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Abstract

Results of studying im**ement of a supersonic underexpanded air jet onto a finite-thickness porous metal obstacle whose frontal plane is normal to the jet axis and whose side surface is impermeable for the gas flow are reported. The case of a non-porous obstacle of the same diameter is considered for determining the effect of porosity on gas-dynamic characteristics of jet–obstacle interaction.

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Correspondence to V. I. Zapryagaev.

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Original Russian Text © V.I. Zapryagaev, I.N. Kavun, A.V. Solotchin.

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 56, No. 3, pp. 73–81, May–June, 2015.

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Zapryagaev, V.I., Kavun, I.N. & Solotchin, A.V. Flow structure formed due to interaction of a supersonic jet with a porous obstacle. J Appl Mech Tech Phy 56, 406–413 (2015). https://doi.org/10.1134/S0021894415030098

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  • DOI: https://doi.org/10.1134/S0021894415030098

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