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Two-phase reacting flow induced by a sufficiently strong shock wave impacting on an interface of combustible dust suspension at an angle of 0?or passing over a combustible dust deposit at an angle of 90° has been investigated experimentally and numerically.The.onset and development processes of interactions have been discussed according to the results reported.Computed and measured results are in reasonable agreement.
Two-phase reacting flow induced by a strong strong shock wave impacting on an interface of combustible dust suspension at an angle of 0? Or passing over a combustible dust deposit at an angle of 90 ° has been investigated experimentally and numerically. development processes of interactions have been discussed according to the results reported. Computed and measured results are in reasonable agreement.