In this study four different supersonic nozzles circular, elliptical, tabbe
d, and radially lobed nozzles are compared experimentally for their freejet
mixing performance. With the background of studies by various groups condu
cted on elliptical, tabbed, and radially lobed nozzles, the present paper a
ims at a comparative experimental study to compare their mixing performance
with that of a conventional circular nozzle under identical operating cond
itions. The investigation is performed non-intrusively, using digital image
processing of the planar Mie scattering images of the flow field. The resu
lts of these investigations reveal the superiority of the mixing performanc
e of the lobed nozzles over conventional circular and other non-conventiona
l nozzles.