%0 Journal Article
%T PENETRATION OF A SHOCK WAVE IN A FULLY SUPERSONIC FLAME FRONT WITH THE FORMATION OF AN EXPANSION FAN
%A Dan PANTAZOPOL
%J INCAS Bulletin
%D 2011
%I National Institute for Aerospace Research ˇ°Elie Carafoliˇ± - INCAS
%R 10.13111/2066-8201.2011.3.1.10
%X In a previous paper [3] was treated the ,,simple penetrationˇ± of an incident shock wavethrough a fully supersonic flame front in the space of the hot burnt gases, situated in a supersonictwo-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 theinterference phenomena.
%K shock waves
%K flame front
%K expansion fan
%U http://bulletin.incas.ro/files/dan_pantazopol_v3is1_full.pdf