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In a previous paper (3) was treated the ,,simple penetration" of an incident shock wave through a fully supersonic flame front in the space of the hot burnt gases, situated in a supersonic two-dimensional flow of an ideal homogeneous /combustible gas was treated in a previous paper (3). In the present paper takes into consideration, a configuration, in which an expansion fan is produced, is take into consideration the shock polar and expansion polar are used for the analyze of the interference phenomena.

PENETRATION OF A SHOCK WAVE IN A FULLY SUPERSONIC FLAME FRONT WITH THE FORMATION OF AN EXPANSION FAN