GT2021-60012 Compressor Maps and Coupling: Symmetry, Paradox, and Clarity

GT2021-60012 Compressor Maps and Coupling: Symmetry, Paradox, and Clarity

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:ASME Turbo Expo (2021 : Online) Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition ; Volume 2, A: Turbomachinery: Axial flow fan and compressor aerodynamics
1. Verfasser: Iwrey, Benjamin (VerfasserIn)
Pages:2021
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
GT2021-01771 Development of Loss Correlation and Tool Validation at Transonic Condition Based on Cascade Test 2021 Choi, Jaewoo
GT2021-58665 Highly Resolved Simulations of a CDA Compressor Cascade: Effect of Reynolds Number on Losses 2021 Leggett, John
GT2021-58676 Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part I: Methodology and Computational Results 2021 Lee, Jinwook
GT2021-58742 Endwall Boundary Layer Development in a Multistage Low-Speed Compressor With Tandem Stator Vanes 2021 Hopfinger, Michael
GT2021-58793 Effects of Rotation on the Flow Structure in a Compressor Cascade 2021 Ventosa-Molina, Jordi
GT2021-58941 Composite UHBR Fan for Forced Response and Flutter Investigations 2021 Eggers, Torben
GT2021-58940 Design and Pre-Test Evaluation of a Low-Pressure Compressor Test Facility for Cryogenic Hydrogen Fuel Integration 2021 Jonsson, Isak
GT2021-59186 Low-Pressure Compressor Near-Stall Predictions Using Unsteady CFD Methods 2021 Vanpouille, David
GT2021-59284 Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade 2021 Liu, Qiang
GT2021-59452 Aerodynamic Mitigation of Mechanical Constraints in Small Compressor Blade Profiles 2021 Dickens, Tony
GT2021-59589 Comprehensive Performance Improvement for a 16-Stage Axial Compressor 2021 Popov, Grigorii
GT2021-59899 Experimental Study on Different Tip Clearance of Low-Speed Axial Fan 2021 Zhang, Ming
GT2021-60115 Jetails of Shrouded Stator Hub Cavity Flow in a Multi-Stage Axial Compressor Part 2: Leakage Flow Characteristics in Stator Wells 2021 Kamdar, Nitya
GT2021-01098 Evaluation of a Flow Measurement Probe Influence on the Flow Field in High Speed Axial Compressors 2021 Seki, Ryosuke
GT2021-58678 Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss — Part Il: Experimental Assessments and Applications 2021 Lee, Jinwook
GT2021-58745 Flow Physics in a Large Rotor Tip Gap in a Multi-Stage Axial Compressor 2021 Hah, Chunill
GT2021-58798 Performance Evaluation of Leading Edge Tubercles Applied to the Blades in a 2-D Compressor Cascade 2021 Sidhu, Satpreet S.
GT2021-59047 Effects of Probe Stem Surface Suction on the Aerodynamic Performance of a Compressor 2021 Zhong, Yafei
GT2021-539182 Effect of an Axially Tilted Variable Stator Vane Platform on Penny Cavity and Main Flow 2021 Janssen, Johannes
GT2021-59851 An Experimental Investigation Into the Impacts of Varying the Circumferential Extent of Tip-Low Total Pressure Distortion on Fan Stability 2021 Allen, Oliver
Alle Artikel auflisten