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    Effect of Vortex Generators on Film Cooling Effectiveness

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 006::page 61009
    Author:
    Sarkar, S.
    ,
    Ranakoti, Ganesh
    DOI: 10.1115/1.4035275
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling is often adopted, where coolant jets are ejected to form a protective layer on the surface against the hot combustor gases. The bending of jets in crossflow results in counter rotating vortex pair (CRVP), which is a cause for high jet lift-off and poor film cooling effectiveness in the near field. There are efforts to mitigate this detrimental effect of CRVP, and thus, to improve the film cooling performance. In the present study, the effects of both downwash and upwash type of vortex generator (VG) on film cooling are numerically analyzed. A series of discrete holes on a flat plate with 35 deg streamwise orientation and connected to a common delivery plenum is used here, where the vortex generators are placed upstream of the holes. The blowing ratio and the density ratio are considered as 0.5 and 1.2, respectively, with a Reynolds number based on freestream velocity and diameter of hole being 15,885. The computations are performed by ANSYS fluent 13.0 using k–ε realizable turbulence model. The results show that vortices generated by downwash vortex generator (DWVG) counteracts the effect of CRVP preventing the jet lift-off, which results in increased effectiveness in streamwise as well as in spanwise directions. However, upwash vortex generator (UWVG) augments the effect of CRVP, resulting in poor performance of film cooling.
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      Effect of Vortex Generators on Film Cooling Effectiveness

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    contributor authorSarkar, S.
    contributor authorRanakoti, Ganesh
    date accessioned2017-11-25T07:19:52Z
    date available2017-11-25T07:19:52Z
    date copyright2017/7/2
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_06_061009.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236072
    description abstractFilm cooling is often adopted, where coolant jets are ejected to form a protective layer on the surface against the hot combustor gases. The bending of jets in crossflow results in counter rotating vortex pair (CRVP), which is a cause for high jet lift-off and poor film cooling effectiveness in the near field. There are efforts to mitigate this detrimental effect of CRVP, and thus, to improve the film cooling performance. In the present study, the effects of both downwash and upwash type of vortex generator (VG) on film cooling are numerically analyzed. A series of discrete holes on a flat plate with 35 deg streamwise orientation and connected to a common delivery plenum is used here, where the vortex generators are placed upstream of the holes. The blowing ratio and the density ratio are considered as 0.5 and 1.2, respectively, with a Reynolds number based on freestream velocity and diameter of hole being 15,885. The computations are performed by ANSYS fluent 13.0 using k–ε realizable turbulence model. The results show that vortices generated by downwash vortex generator (DWVG) counteracts the effect of CRVP preventing the jet lift-off, which results in increased effectiveness in streamwise as well as in spanwise directions. However, upwash vortex generator (UWVG) augments the effect of CRVP, resulting in poor performance of film cooling.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Vortex Generators on Film Cooling Effectiveness
    typeJournal Paper
    journal volume139
    journal issue6
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4035275
    journal fristpage61009
    journal lastpage061009-11
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 006
    contenttypeFulltext
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