Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)

The laminar-turbulent transition of a boundary layer induced by a jet injection in the inlet region of a circular pipe was experimentally investigated. The jet was periodically injected radially from a small hole in the inlet region into the pipe flow. Axial velocity was measured by a hot-wire anemo...

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Main Authors: Masashi ICHIMIYA, Hayato MATSUDAIRA, Hayato FUJIMURA, Hideki OHNO
Format: Article
Language:English
Published: The Japan Society of Mechanical Engineers 2013-12-01
Series:Journal of Fluid Science and Technology
Subjects:
Online Access:https://www.jstage.jst.go.jp/article/jfst/8/3/8_436/_pdf/-char/en
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author Masashi ICHIMIYA
Hayato MATSUDAIRA
Hayato FUJIMURA
Hideki OHNO
author_facet Masashi ICHIMIYA
Hayato MATSUDAIRA
Hayato FUJIMURA
Hideki OHNO
author_sort Masashi ICHIMIYA
collection DOAJ
description The laminar-turbulent transition of a boundary layer induced by a jet injection in the inlet region of a circular pipe was experimentally investigated. The jet was periodically injected radially from a small hole in the inlet region into the pipe flow. Axial velocity was measured by a hot-wire anemometer. The turbulence induced by the jet within the boundary layer developed into turbulent patches which then grew in the axial, circumferential and radial directions downstream. The shape of the patches shown by the intermittency factor in the diametrical plane was similar to the turbulent spot in the flat plate boundary layer at first, then became similar to the turbulent slug in the pipe flow developed downstream. The turbulent patches protruded from the boundary layer after they grew and reached the circumferential opposite side, although they stayed within the boundary layer as long as the shape was turbulent spot-like in the diametrical plane. The propagation velocity at the leading edge became faster than the cross-sectional velocity, though it turned slower at the trailing edge. Therefore, the growth rate of its axial length varied downstream. The growth rate of the patches' circumferential length was smaller than that in the turbulent spot under zero pressure gradient and was almost the same as the spot under favorable pressure gradient.
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spelling doaj.art-b965c19d566b43399b5cbff0a77befe22022-12-21T21:19:53ZengThe Japan Society of Mechanical EngineersJournal of Fluid Science and Technology1880-55582013-12-018343645110.1299/jfst.8.436jfstLaminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)Masashi ICHIMIYA0Hayato MATSUDAIRA1Hayato FUJIMURA2Hideki OHNO3Institute of Technology and Science, The University of TokushimaGraduate School, The University of TokushimaGraduate School, The University of TokushimaGraduate School, The University of TokushimaThe laminar-turbulent transition of a boundary layer induced by a jet injection in the inlet region of a circular pipe was experimentally investigated. The jet was periodically injected radially from a small hole in the inlet region into the pipe flow. Axial velocity was measured by a hot-wire anemometer. The turbulence induced by the jet within the boundary layer developed into turbulent patches which then grew in the axial, circumferential and radial directions downstream. The shape of the patches shown by the intermittency factor in the diametrical plane was similar to the turbulent spot in the flat plate boundary layer at first, then became similar to the turbulent slug in the pipe flow developed downstream. The turbulent patches protruded from the boundary layer after they grew and reached the circumferential opposite side, although they stayed within the boundary layer as long as the shape was turbulent spot-like in the diametrical plane. The propagation velocity at the leading edge became faster than the cross-sectional velocity, though it turned slower at the trailing edge. Therefore, the growth rate of its axial length varied downstream. The growth rate of the patches' circumferential length was smaller than that in the turbulent spot under zero pressure gradient and was almost the same as the spot under favorable pressure gradient.https://www.jstage.jst.go.jp/article/jfst/8/3/8_436/_pdf/-char/enpipe flowtransitionboundary layerturbulenceinlet regionisolated turbulent patchpropagation velocityturbulent spot
spellingShingle Masashi ICHIMIYA
Hayato MATSUDAIRA
Hayato FUJIMURA
Hideki OHNO
Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
Journal of Fluid Science and Technology
pipe flow
transition
boundary layer
turbulence
inlet region
isolated turbulent patch
propagation velocity
turbulent spot
title Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
title_full Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
title_fullStr Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
title_full_unstemmed Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
title_short Laminar-Turbulent Transition of an Inlet Boundary Layer in a Circular Pipe Induced by Periodic Injection (Shape of Isolated Turbulent Patches and Their Growth)
title_sort laminar turbulent transition of an inlet boundary layer in a circular pipe induced by periodic injection shape of isolated turbulent patches and their growth
topic pipe flow
transition
boundary layer
turbulence
inlet region
isolated turbulent patch
propagation velocity
turbulent spot
url https://www.jstage.jst.go.jp/article/jfst/8/3/8_436/_pdf/-char/en
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