GT2021-59661 Numerical Study of Droplet Erosion in the First-Stage Rotor of an Axial Flow Compressor

GT2021-59661 Numerical Study of Droplet Erosion in the First-Stage Rotor of an Axial Flow Compressor

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, B: Turbomachinery: Axial flow turbine aerodynamics; deposition, erosion, fouling, and icing
1. Verfasser: Agatıi, Giuliano (VerfasserIn)
Weitere Verfasser: Borello, Domenico (VerfasserIn), Gruttola, Francesca Di (VerfasserIn), Rispoli, Franco (VerfasserIn), Venturini, Paolo (VerfasserIn), Gabriele, Serena (VerfasserIn), Simone, Domenico (VerfasserIn)
Pages:2021
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
GT2021-58563 Simulation of Passing Wakes Inducing Unsteady Boundary Layer Transition Around Low-Pressure Turbine Blade 2021 Dufau, Antoine
GT2021-58995 High-Fidelity Simulations of a High-Pressure Turbine Stage: Effects of Reynolds Number and Inlet Turbulence 2021 Zhao, Yaomin
GT2021-59219 Design and Testing of a Multi-Stage IP Turbine for Future Geared Turbofans 2021 Torre, D.
GT2021-59224 Experimental and Numerical Flow Analysis of an Engine-Realistic State-of-the-Art Turbine Rear Structure 2021 Vikhorev, Valentin
GT2021-58673 Data-Driven Analysis of Engine Mission Severity Using Non-Dimensional Groups 2021 Brandes, Tim
GT2021-58816 High-Fidelity Simulations of a High-Pressure Turbine Vane With End Walls: Impact of Secondary Structures and Spanwise Temperature Profiles on Losses 2021 Zhao, Yaomin
GT2021-59694 The Effect of Inlet Conditions on Turbine Endwall Loss 2021 Coull, John D.
GT2021-59701 Vortex Tracking of Purge-Mainstream Interactions in a Rotating Turbine Stage 2021 Mesny, Alex W.
GT2021-59897 Effect of Microcylinder and D-Cylinder at the Leading Edge of a Wells Turbine Harvesting Wave Energy 2021 Sadees, P.
GT2021-59112 Evaluating the influence of Rotor-Casing Eccentricity on Turbine Efficiency Including Time-Resolved Flow Field Measurements 2021 DeShong, Eric T.
GT2021-59192 Influence of Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient and Low Freestream Turbulence 2021 Jeong, Heechan
GT2021-59606 Numerical Investigation of Loss Development in a Low-Pressure Turbine Cascade With Unsteady Inflow and Varying Infet Endwail Boundary Layer 2021 Schubert, Tobias
GT2021-58477 A Discrete Element Methods-Based Model for Particulate Deposition and Rebound in Gas Turbines 2021 Gaskell, Jack G.
GT2021-58887 A Key Flow Parameter to the Profile Loss of Low-Pressure Turbine Blades 2021 Kodama, Hidekazu
GT2021-59388 Determining Total Pressure Fields From Velocimetry Measurements in a Transonic Turbine Flowfield 2021 Rusted, Alexander
GT2021-60013 Development of Turbulent Quantities Inside an Axial Turbine Vane 2021 Behre, Stephan
GT2021-60224 Ehancing Turbine Deposition Prediction Capability With Conjugate Mesh Morprning 2021 Bowen, Christopher P.
GT2021-59661 Numerical Study of Droplet Erosion in the First-Stage Rotor of an Axial Flow Compressor 2021 Agatıi, Giuliano
Alle Artikel auflisten