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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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    Loss Prediction in an Axial Compressor Cascade at Off-Design Incidences With Free Stream Disturbances Using Large Eddy Simulation 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 007:;page 71005
    Author(s): Leggett, John; Priebe, Stephan; Shabbir, Aamir; Michelassi, Vittorio; Sandberg, Richard; Richardson, Edward
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Axial compressors may be operated under off-design incidences due to variable operating conditions. Therefore, a successful design requires accurate performance and stability limits predictions under a wide operating range. ...
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    Loss Analysis of Unsteady Turbomachinery Flows Based on the Mechanical Work Potential 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 011:;page 0111009-1
    Author(s): Leggett, John; Richardson, Edward; Priebe, Stephan; Shabbir, Aamir; Michelassi, Vittorio; Sandberg, Richard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Loss analysis is a valuable technique for improving the thermodynamic performance of turbomachines. Analyzing loss in terms of the “mechanical work potential” (Miller, R.J., ASME Turbo Expo 2013, GT2013-95488) provides an ...
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