Show simple item record

contributor authorStratton, Zachary T.
contributor authorShih, Tom I-P.
date accessioned2019-02-28T11:09:57Z
date available2019-02-28T11:09:57Z
date copyright9/28/2018 12:00:00 AM
date issued2018
identifier issn0889-504X
identifier otherturbo_140_10_101007.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253367
description abstractLarge eddy simulations (LES) were performed to investigate film cooling of a flat plate, where the cooling jets issued from a plenum through one row of circular holes of diameter D and length 4.7D that are inclined at 35 deg relative to the plate. The focus is on understanding the turbulent structure of the film-cooling jet and the film-cooling effectiveness. Parameters studied include blowing ratio (BR = 0.5 and 1.0) and density ratio (DR = 1.1 and 1.6). Also, two different boundary layers (BL) upstream of the film-cooling hole were investigated—one in which a laminar BL was tripped to become turbulent from near the leading edge of the flat plate, and another in which a mean turbulent BL is prescribed directly. The wall-resolved LES solutions generated were validated by comparing its time-averaged values with data from PIV and thermal measurements. Results obtained show that having an upstream BL that does not have turbulent fluctuations enhances the cooling effectiveness significantly at low velocity ratios (VR) when compared to an upstream BL that resolved the turbulent fluctuations. However, these differences diminish at higher VRs. Instantaneous flow reveals a bifurcation in the jet vorticity as it exits the hole at low VRs, one branch forming the shear-layer vortex, while the other forms the counter-rotating vortex pair (CRVP). At higher VRs, the shear layer vorticity is found to reverse direction, changing the nature of the turbulence and the heat transfer. Results obtained also show the strength and structure of the turbulence in the film-cooling jet to be strongly correlated to VR.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Density and Blowing Ratios on the Turbulent Structure and Effectiveness of Film Cooling
typeJournal Paper
journal volume140
journal issue10
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4041218
journal fristpage101007
journal lastpage101007-12
treeJournal of Turbomachinery:;2018:;volume 140:;issue 010
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record