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    Multiple Jets in a Crossflow: Detailed Measurements and Numerical Simulations

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002::page 330
    Author:
    P. Ajersch
    ,
    J.-M. Zhou
    ,
    S. Ketler
    ,
    M. Salcudean
    ,
    I. S. Gartshore
    DOI: 10.1115/1.2841116
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The fluid mechanics and heat transfer characteristics of film cooling are three-dimensional and highly complex. To understand this problem better, an experimental study was conducted in a low-speed wind tunnel on a row of six rectangular jets injected at 90 deg to the crossflow (mainstream flow). The jet-to-crossflow velocity ratios (blowing ratios) examined were 0.5, 1.0, and 1.5, and the jet spacing-to-jet width ratio was 3.0. No significant temperature difference between jet and crossflow air was introduced. Mean velocities and six flow stresses were measured using a three-component laser-Doppler velocimeter operating in coincidence mode. Seeding of both jet and cross-stream air was achieved with a commercially available smoke generator. Flow statistics are reported in the form of vector plots, contours, and x-y graphs, showing velocity, turbulence intensity, and Reynolds stresses. To complement the detailed measurements, flow visualization was accomplished by transmitting the laser beam through a cylindrical lens, thereby generating a narrow, intense sheet of light. Jet air only was seeded with smoke, which was illuminated in the plane of the light sheet. Therefore, it was possible to record on video tape the trajectory and penetration of the jets in the crossflow. Selected still images from the recordings are presented. Numerical simulations of the observed flow field were made by using a multigrid, segmented, k–ε CFD code. Special near-wall treatment included a nonisotropic formulation for the effective viscosity, a low-Re model for k, and an algebraic model for the length scale. Comparisons between the measured and computed velocities show good agreement for the nonuniform mean flow at the jet exit plane. Velocities and stresses on the jet centerline downstream of the orifice are less well predicted, probably because of inadequate turbulence modeling, while values off the centerline match those of the experiments much more closely.
    keyword(s): Measurement , Computer simulation , Jets , Flow (Dynamics) , Stress , Turbulence , Smoke , Wind tunnels , Fluid mechanics , Viscosity , Lenses (Optics) , Temperature , Heat transfer , Cooling , Lasers , Velocimeters , Flow visualization , Laser beams , Trajectories (Physics) , Computational fluid dynamics , Modeling AND Generators ,
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      Multiple Jets in a Crossflow: Detailed Measurements and Numerical Simulations

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    http://yetl.yabesh.ir/yetl1/handle/yetl/119640
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    • Journal of Turbomachinery

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    contributor authorP. Ajersch
    contributor authorJ.-M. Zhou
    contributor authorS. Ketler
    contributor authorM. Salcudean
    contributor authorI. S. Gartshore
    date accessioned2017-05-08T23:55:11Z
    date available2017-05-08T23:55:11Z
    date copyrightApril, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28659#330_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119640
    description abstractThe fluid mechanics and heat transfer characteristics of film cooling are three-dimensional and highly complex. To understand this problem better, an experimental study was conducted in a low-speed wind tunnel on a row of six rectangular jets injected at 90 deg to the crossflow (mainstream flow). The jet-to-crossflow velocity ratios (blowing ratios) examined were 0.5, 1.0, and 1.5, and the jet spacing-to-jet width ratio was 3.0. No significant temperature difference between jet and crossflow air was introduced. Mean velocities and six flow stresses were measured using a three-component laser-Doppler velocimeter operating in coincidence mode. Seeding of both jet and cross-stream air was achieved with a commercially available smoke generator. Flow statistics are reported in the form of vector plots, contours, and x-y graphs, showing velocity, turbulence intensity, and Reynolds stresses. To complement the detailed measurements, flow visualization was accomplished by transmitting the laser beam through a cylindrical lens, thereby generating a narrow, intense sheet of light. Jet air only was seeded with smoke, which was illuminated in the plane of the light sheet. Therefore, it was possible to record on video tape the trajectory and penetration of the jets in the crossflow. Selected still images from the recordings are presented. Numerical simulations of the observed flow field were made by using a multigrid, segmented, k–ε CFD code. Special near-wall treatment included a nonisotropic formulation for the effective viscosity, a low-Re model for k, and an algebraic model for the length scale. Comparisons between the measured and computed velocities show good agreement for the nonuniform mean flow at the jet exit plane. Velocities and stresses on the jet centerline downstream of the orifice are less well predicted, probably because of inadequate turbulence modeling, while values off the centerline match those of the experiments much more closely.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMultiple Jets in a Crossflow: Detailed Measurements and Numerical Simulations
    typeJournal Paper
    journal volume119
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841116
    journal fristpage330
    journal lastpage342
    identifier eissn1528-8900
    keywordsMeasurement
    keywordsComputer simulation
    keywordsJets
    keywordsFlow (Dynamics)
    keywordsStress
    keywordsTurbulence
    keywordsSmoke
    keywordsWind tunnels
    keywordsFluid mechanics
    keywordsViscosity
    keywordsLenses (Optics)
    keywordsTemperature
    keywordsHeat transfer
    keywordsCooling
    keywordsLasers
    keywordsVelocimeters
    keywordsFlow visualization
    keywordsLaser beams
    keywordsTrajectories (Physics)
    keywordsComputational fluid dynamics
    keywordsModeling AND Generators
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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