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contributor authorAravindh Kumar, S. M.
contributor authorRathakrishnan, E.
date accessioned2017-11-25T07:16:35Z
date available2017-11-25T07:16:35Z
date copyright2017/21/7
date issued2017
identifier issn0098-2202
identifier otherfe_139_10_101103.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4234074
description abstractNozzle aspect ratio effect on the mixing of Mach 2 elliptic free jet, issuing from convergent–divergent elliptic nozzles of aspect ratios 2, 3, and 4, in the presence of adverse and marginally favorable pressure gradients at the nozzle exit has been studied experimentally. The results show that AR4 jet enjoys better mixing than AR2 and AR3 jets at all nozzle pressure ratios. The AR2 and AR3 jets displayed axis switching, whereas there is no axis switching for AR4 jet. The shadowgraph shows that the waves in AR4 jet are weaker than those in AR2 and AR3 jets.
publisherThe American Society of Mechanical Engineers (ASME)
titleNozzle Aspect Ratio Effect on Supersonic Elliptic Jet Mixing
typeJournal Paper
journal volume139
journal issue10
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4036823
journal fristpage101103
journal lastpage101103-17
treeJournal of Fluids Engineering:;2017:;volume( 139 ):;issue: 010
contenttypeFulltext


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