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    Large Eddy Simulation on the Interactions of Wake and Film Cooling Near a Leading Edge 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 001:;page 11005
    Author(s): Sarkar, S.; Babu, Harish
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow physics due to interactions between a separated shear layer and film cooling jet apart from excitation of periodic passing wake are studied using large eddy simulation (LES). An aerofoil of constant ...
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    Effect of Vortex Generators on Film Cooling Effectiveness 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 006:;page 61009
    Author(s): Sarkar, S.; Ranakoti, Ganesh
    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 ...
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    Effects of Free Stream Turbulence on Transition of a Separated Boundary Layer Over the Leading Edge of a Constant Thickness Airfoil 

    Source: Journal of Fluids Engineering:;2016:;volume( 138 ):;issue: 002:;page 21202
    Author(s): Samson, A.; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the change in the transition mechanism of a separated boundary layer formed from the semicircular leadingedge of a constant thickness airfoil as the freestream turbulence (fst) increases. Experiments ...
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    Features of a Laminar Separated Boundary Layer Near the Leading-Edge of a Model Airfoil for Different Angles of Attack: An Experimental Study 

    Source: Journal of Fluids Engineering:;2017:;volume( 139 ):;issue: 002:;page 21201
    Author(s): Anand, K.; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The evolution of a separated boundary layer over a model airfoil with semicircular leading-edge has been illustrated for angles of attack (α) varying from −3 deg to 10 deg, where the Reynolds number (Rec) based on chord ...
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    Excitation of Shear Layer Due to Surface Roughness Near the Leading Edge: An Experiment 

    Source: Journal of Fluids Engineering:;2021:;volume( 143 ):;issue: 005:;page 051301-1
    Author(s): Singh, Pradeep; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, a comprehensive study has been performed to address the excitation of a separated boundary layer near the leading edge due to surface roughness. Experiments are performed on a model airfoil with the semicircular ...
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    Excitation of a Separated Flow by a Series of Protuberances Near the Leading Edge of a Model Aerofoil 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 011:;page 111001-1
    Author(s): Singh, Pradeep; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article documents the manifestation of a shear layer under the excitation of a series of hemispherical protuberances near the leading edge of a constant-thickness airfoil. The experiments are performed at a Reynolds ...
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    Large Eddy Simulation of Self-Sustained Cavity Oscillation for Subsonic and Supersonic Flows 

    Source: Journal of Fluids Engineering:;2017:;volume( 139 ):;issue: 001:;page 11102
    Author(s): Nair, K. M.; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primary objective is to perform a large eddy simulation (LES) using shear improved Smagorinsky model (SISM) to resolve the large-scale structures, which are primarily responsible for shear layer oscillations and acoustic ...
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    Interactions of Separation Bubble With Oncoming Wakes by Large Eddy Simulation 

    Source: Journal of Heat Transfer:;2016:;volume( 138 ):;issue: 002:;page 21703
    Author(s): Sarkar, S.; Babu, Harish; Sadique, Jasim
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow physics and heat transfer characteristics due to interactions of periodic passing wakes with a separated boundary layer are studied using largeeddy simulation (LES). A series of airfoils of constant ...
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    Diurnal Warm Layers in the Ocean: Energetics, Nondimensional Scaling, and Parameterization 

    Source: Journal of Physical Oceanography:;2024:;volume( 054 ):;issue: 004:;page 1037
    Author(s): Schmitt, M.; Pham, H. T.; Sarkar, S.; Klingbeil, K.; Umlauf, L.
    Publisher: American Meteorological Society
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    Computation of the Flow Over a Sphere at Re = 3700: A Comparison of Uniform and Turbulent Inflow Conditions 

    Source: Journal of Applied Mechanics:;2014:;volume( 081 ):;issue: 012:;page 121003
    Author(s): Bazilevs, Y.; Yan, J.; de Stadler, M.; Sarkar, S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A highly resolved computation of the flow past a sphere at Reynolds number Re = 3700 using a finite element method (FEM)based residualbased variational multiscale (RBVMS) formulation is performed. Both uniform and ...
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