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Deflagration-to-detonation transition in crossed-flow fast jets of propellant components

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Abstract

It was experimentally proven for the first time that the turbulence produced by crossed-flow supersonic jets of a fuel (natural gas) and an oxidizer (oxygen), which are injected at a pressure of 25 to 150 atm into a smooth detonation tube 74 mm in diameter, causes a fast deflagration-to-detonation transition at distances as short as 300 mm (up to 4 tube diameters) in times of tenths of a millisecond (∼0.4 ms). The obtained results can be used for designing compact predetonators for detonation combustors of promising energy-converting devices.

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Correspondence to S. M. Frolov.

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Original Russian Text © S.M. Frolov, V.A. Smetanyuk, V.S. Aksenov, A.S. Koval’, 2017, published in Doklady Akademii Nauk, 2017, Vol. 476, No. 1, pp. 59–62.

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Frolov, S.M., Smetanyuk, V.A., Aksenov, V.S. et al. Deflagration-to-detonation transition in crossed-flow fast jets of propellant components. Dokl Phys Chem 476, 153–156 (2017). https://doi.org/10.1134/S0012501617090019

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  • DOI: https://doi.org/10.1134/S0012501617090019

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