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    Geometric and Flow Characterization of Additively Manufactured Turbine Blades With Drilled Film Cooling Holes 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41013-1
    Author(s): McCormack, Kelsey E.; Rozman, Maria; Berdanier, Reid A.; Thole, Karen A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As designers investigate new cooling technologies to advance future gas turbine engines, manufacturing methods that are fast and accurate are needed. Additive manufacturing facilitates the rapid prototyping of parts at a ...
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    Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 010:;page 101009-1
    Author(s): Rozman, Maria; Berdanier, Reid A.; Barringer, Michael D.; Thole, Karen A.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbines are used in a broad range of aerospace and land-based applications from power generation to aviation, and their usage is projected to continue to grow. It is therefore critical to improve turbine efficiency ...
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    Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 003:;page 31014-1
    Author(s): Rozman, Maria; DeShong, Eric T.; Thole, Karen A.; Berdanier, Reid A.; Robak, Christopher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine engine design requires considerations not only for long-term steady operation but also for critical transient events. Aircraft engines undergo significant stress during takeoff and landing, while power generation ...
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