The set of experiments in tube (filled by H2-air mixtures) with partially obstructed area and multidimensional endplate was done. Three main regimes of loading from explosive combustion of H2+air mixtures nearby obstructed area were distinguished on the basis of tests performed. The interaction of a decaying complex shock wave+decelerating flame front emitted from obstacled section with concave reflector gives rise to secondary explosion waves from hot exothermic centers inside non-flat reflecyor at H2 concentration in range (15%--20%) vol.
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