“…For example, the freestream remains supersonic in the combustor, so mixing of fuel jets with the freestream must be quick. Some injection schemes to enhance the mixing for the SCRAMJET have been suggested, [2][3][4][5][6][7][8][9][10][11] such as wedge shaped injector schemes 2,3) and their derivations, 4,5) rampinjector schemes 6,7) and their derivations 8,9) and inclined-injector schemes. 10,11) It is important to evaluate the mixing condition in the SCRAMJET in order to suggest or develop these injection schemes.…”