Show simple item record

contributor authorKuchana
contributor authorVinayender;Balakrishnan
contributor authorN.;Srinivasan
contributor authorBalamurugan
date accessioned2022-08-18T12:57:42Z
date available2022-08-18T12:57:42Z
date copyright6/2/2022 12:00:00 AM
date issued2022
identifier issn0742-4795
identifier othergtp_144_08_085001.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287174
description abstractThe use of splitter blade as a passive flow control mechanism in the design of separation free aggressive annular diffuser is explored through computational fluid dynamics simulations. The fundamental working principle of a splitter blade in case of a two-dimensional rectangular diffuser and an annular diffuser is discussed. The effects of splitter blade configuration on the end-wall adverse pressure gradients are discussed. An aggressive diffuser design space is identified with ducts of maximum slope of 50 deg and maximum divergence angle between the outer and inner walls of 10 deg for axial-length to inlet height ratio ranging from 1.25 to 2.5. One or more splitter blades are employed in the duct to eliminate flow separation for all the ducts in the aggressive design space considered. Requirement of number of splitter blades in the aggressive design space is demarcated. Performance charts for the ducts in this aggressive design space are also established.
publisherThe American Society of Mechanical Engineers (ASME)
titleDesign of Curved Annular Diffusers II: Using Splitter Blades
typeJournal Paper
journal volume144
journal issue8
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4054580
journal fristpage85001-1
journal lastpage85001-17
page17
treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 008
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record