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    Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part I: Methodology and Challenges 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31008-1
    Author(s): Nardini, Massimiliano; Kozul, Melissa; Jelly, Thomas O.; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-fidelity simulation of transitional and turbulent flows over multi-scale surface roughness presents several challenges. For instance, the complex and irregular geometrical nature of surface roughness makes it impractical ...
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    Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305) 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81020-1
    Author(s): Kozul, Melissa; Nardini, Massimiliano; Przytarski, Pawel J.; Solomon, William; Shabbir, Aamir; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Streamwise micro-groove surfaces (“riblets”) are well known as a passive surface treatment to reduce drag, which may assist in increasing overall gas turbine efficiency. The first direct numerical simulation of micro-scaled ...
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    Effects of Localized Non-Gaussian Roughness on High-Pressure Turbine Aerothermal Performance: Convective Heat Transfer, Skin Friction, and the Reynolds’ Analogy 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 005:;page 51017-1
    Author(s): Jelly, Thomas O.; Nardini, Massimiliano; Sandberg, Richard D.; Vitt, Paul; Sluyter, Greg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressible direct numerical simulations are conducted to investigate how surface roughness affects the aerothermal performance of a high-pressure turbine vane operating at an exit Reynolds number of 0.59 ×106 and exit ...
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    Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part II: The Effect of Roughness on the Performance of a High-Pressure Turbine Blade 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31009-1
    Author(s): Nardini, Massimiliano; Jelly, Thomas O.; Kozul, Melissa; Sandberg, Richard D.; Vitt, Paul; Sluyter, Greg
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blades generally present surface roughness introduced in the manufacturing process or caused by in-service degradation, which can have a significant impact on aero-thermal performance. A better understanding of the ...
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    Effects of Riblet Dimensions on the Transitional Boundary Layers Over High-Lift Turbine Blades 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31012-1
    Author(s): Ananth, S. M.; Nardini, Massimiliano; Vaid, Aditya; Kozul, Melissa; Rao Vadlamani, Nagabhushana; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Substantial research exists in the literature on reducing the profile loss of transitional boundary layers over low-pressure turbine (LPT) blades via different mechanisms such as freestream turbulence, upstream wakes, and ...
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    Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41011-1
    Author(s): Ananth, S. M.; Nardini, Massimiliano; Kozul, Melissa; Vadlamani, Nagabhushana Rao; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent research has demonstrated the effectiveness of riblets (streamwise aligned grooves) in reducing the profile loss of low-pressure turbine (LPT) blades under high-lift (HL) loading. In this research, we pursue the ...
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    Profile Loss Reduction of High-Lift Turbine Blades With Rough and Ribbed Surfaces 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002:;page 21001-1
    Author(s): Sivaramakrishnan Malathi, Ananth; Nardini, Massimiliano; Vaid, Aditya; Rao Vadlamani, Nagabhushana; Sandberg, Richard D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transitional boundary layers on low-pressure turbines (LPTs) are prone to separation on the suction surface of the blade under strong local adverse pressure gradients. Intermittent freestream turbulence, periodic wakes ...
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