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Investigation of the structure of a diffusion hydrogen plume in a supersonic high-enthalpy air jet

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Combustion, Explosion and Shock Waves Aims and scope

Abstract

The results of investigation of the plume structure in the case of diffusion combustion of hydrogen in a cocurrent supersonic high-enthalpy off-design air jet are presented. Based on the registration of radiation within the wavelength range of 260–350 nm across and along the flame, a three-dimensional tomographic reconstruction of the plume was obtained, which confirmed the interrelation between the gas-dynamic structure and combustion intensity. A possibility of existence of combustion regimes with periodically repeated cycles of complete extinction and subsequent ignition of hydrogen in accordance with the barrel-shaped structure of the off-design jet is established experimentally. The existence of local peripheral regions of combustion is noted, which can indicate the presence of vortex structures. In the three-dimensional representation (obtained under the assumption of axial symmetry of radiation), these vortex structures have the form of annular zones. In a real flow, helical structures are possibly formed at the plume periphery.

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Translated fromFizika Goreniya i Vzryva, Vol. 35, No. 5, pp. 3–5, September–October 1999.

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Vorontsov, S.S., Zabaikin, V.A., Pikalov, V.V. et al. Investigation of the structure of a diffusion hydrogen plume in a supersonic high-enthalpy air jet. Combust Explos Shock Waves 35, 465–467 (1999). https://doi.org/10.1007/BF02674487

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  • DOI: https://doi.org/10.1007/BF02674487

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