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contributor authorCheng
contributor authorYong, Shan
contributor authorJing
date accessioned2017-05-09T01:07:39Z
date available2017-05-09T01:07:39Z
date issued2014
identifier issn1528-8919
identifier othergtp_136_06_061504.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154717
description abstractThe internal flow characteristics inside lobed mixerejector with curved mixing duct and the parametric effects on the lobed mixerejector performance are investigated numerically and validated by experimental test. The curved mixing duct affects the development of the streamwise vortices induced by the lobed mixer. When the mixing process undergoes the transition from the straight section to the bent section, the flow inside the curved mixing duct is dominated by the impinging and centrifugal effects. In general, the pumping ratio is decreased approximately 20%–30% once the bent section is mounted on the straight duct. The mixerejector performance could by improved by increasing the straight section length, due to more fully momentum utilization of primary jet and weaker influence of bent section on the back pressure near nozzle exit. The mixerejector pumping capacity is also augmented with the increase of mixing duct area ratio until the area ratio is reached to 3.5. And the fullyutilization of primary jet momentum inside mixing duct with big area ratio needs long mixing distance. The pumping ratio is decreased as the increase of bent angle of curved mixing duct in approximately linear relationship. When the bent angle exceeds 45 deg, the thermal mixing efficiency is decreased rapidly as the increase of bent angle.
publisherThe American Society of Mechanical Engineers (ASME)
titleParametric Effects on Internal Aerodynamics of Lobed Mixer Ejector With Curved Mixing Duct
typeJournal Paper
journal volume136
journal issue6
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4026426
journal fristpage61504
journal lastpage61504
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 006
contenttypeFulltext


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