Effect of shock interactions on mixing layer between co-flowing supersonic flows in a confined duct
Sign Up to like & getrecommendations! Published in 2018 at "Shock Waves"
DOI: 10.1007/s00193-017-0722-z
Abstract: Experiments are conducted to observe the effect of shock interactions on a mixing layer generated between two supersonic streams of Mach number M$$_\mathrm {1}$$1 $$=$$= 1.76 and M$$_\mathrm {2}$$2 $$=$$= 1.36 in a confined duct. The development of this… read more here.
Keywords: mixing layer; duct; effect shock; shock interactions ... See more keywords