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    Fan–Intake Interaction Under High Incidence

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 004::page 41204
    Author:
    Cao, Teng
    ,
    Vadlamani, Nagabhushana Rao
    ,
    Tucker, Paul G.
    ,
    Smith, Angus R.
    ,
    Slaby, Michal
    ,
    Sheaf, Christopher T. J.
    DOI: 10.1115/1.4034701
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we present an extensive numerical study on the interaction between the downstream fan and the flow separating over an intake under high incidence. The objectives of this investigation are twofold: (a) to gain qualitative insight into the mechanism of fan–intake interaction and (b) to quantitatively examine the effect of the proximity of the fan on the inlet distortion. The fan proximity is altered using the key design parameter, L/D, where D is the diameter of the intake, and L is the distance of the fan from the intake lip. Both steady and unsteady Reynolds-averaged numerical simulations (RANS) were carried out. For the steady calculations, a low-order fan model has been used, while a full 3D geometry has been used for the unsteady RANS. The numerical methodology is also thoroughly validated against the measurements for the intake-only and fan-only configurations on a high bypass ratio turbofan intake and fan, respectively. To systematically study the effect of fan on the intake separation and explore the design criteria, a simplified intake–fan configuration has been considered. In this fan–intake model, the proximity of the fan to the intake separation (L/D) can be conveniently altered without affecting other parameters. The key results indicate that, depending on L/D, the fan has either suppressed the level of the postseparation distortion or increased the separation-free operating range. At the lowest L/D (∼0.17), around a 5 deg increase in the separation-free angle of incidence was achieved. This delay in the separation-free angle of incidence decreased with increasing L/D. At the largest L/D (∼0.44), the fan was effective in suppressing the postseparation distortion rather than entirely eliminating the separation. Isentropic Mach number distribution over the intake lip for different L/D's revealed that the fan accelerates the flow near the casing upstream of the fan face, thereby decreasing the distortion level in the immediate vicinity. However, this acceleration effect decayed rapidly with increasing upstream distance from the fan-face.
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      Fan–Intake Interaction Under High Incidence

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4233652
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorCao, Teng
    contributor authorVadlamani, Nagabhushana Rao
    contributor authorTucker, Paul G.
    contributor authorSmith, Angus R.
    contributor authorSlaby, Michal
    contributor authorSheaf, Christopher T. J.
    date accessioned2017-11-25T07:15:45Z
    date available2017-11-25T07:15:45Z
    date copyright2016/2/11
    date issued2017
    identifier issn0742-4795
    identifier othergtp_139_04_041204.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4233652
    description abstractIn this paper, we present an extensive numerical study on the interaction between the downstream fan and the flow separating over an intake under high incidence. The objectives of this investigation are twofold: (a) to gain qualitative insight into the mechanism of fan–intake interaction and (b) to quantitatively examine the effect of the proximity of the fan on the inlet distortion. The fan proximity is altered using the key design parameter, L/D, where D is the diameter of the intake, and L is the distance of the fan from the intake lip. Both steady and unsteady Reynolds-averaged numerical simulations (RANS) were carried out. For the steady calculations, a low-order fan model has been used, while a full 3D geometry has been used for the unsteady RANS. The numerical methodology is also thoroughly validated against the measurements for the intake-only and fan-only configurations on a high bypass ratio turbofan intake and fan, respectively. To systematically study the effect of fan on the intake separation and explore the design criteria, a simplified intake–fan configuration has been considered. In this fan–intake model, the proximity of the fan to the intake separation (L/D) can be conveniently altered without affecting other parameters. The key results indicate that, depending on L/D, the fan has either suppressed the level of the postseparation distortion or increased the separation-free operating range. At the lowest L/D (∼0.17), around a 5 deg increase in the separation-free angle of incidence was achieved. This delay in the separation-free angle of incidence decreased with increasing L/D. At the largest L/D (∼0.44), the fan was effective in suppressing the postseparation distortion rather than entirely eliminating the separation. Isentropic Mach number distribution over the intake lip for different L/D's revealed that the fan accelerates the flow near the casing upstream of the fan face, thereby decreasing the distortion level in the immediate vicinity. However, this acceleration effect decayed rapidly with increasing upstream distance from the fan-face.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFan–Intake Interaction Under High Incidence
    typeJournal Paper
    journal volume139
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4034701
    journal fristpage41204
    journal lastpage041204-10
    treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 004
    contenttypeFulltext
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