GT2021-59047 Effects of Probe Stem Surface Suction on the Aerodynamic Performance of a 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, A: Turbomachinery: Axial flow fan and compressor aerodynamics
1. Verfasser: Zhong, Yafei (VerfasserIn)
Weitere Verfasser: Ma, Hongwei (VerfasserIn), Yang, Yi (VerfasserIn)
Pages:2021
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2021
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
GT2021-58457 In-Stall Compressor Performance and the Effects of Reynolds Number 2021 Hutchings, Jack
A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades 2021 Banjac, Milan
GT2021-58657 Numerical Investigation of the Aerodynamic Performance of Hybrid Aerofoils in a 1.5-Stage Low-Speed Compressor 2021 Eckel, Jannik
GT2021-58708 Performance of a Subsonic Compressor Airfoil With Upstream, End-Wall Injection Flow 2021 Pope, Aaron J.
GT2021-58823 Mechanism Analysis of the Influence of Blade Thickness Deviation on The Performance of Axial Flow Compressor 2021 Ji, Tianyuan
GT2021-59007 Effect of Differential Tip Clearance on the Performance of a Tandem Rotor 2021 Kumar, Amit
GT2021-59108 Global Optimisation of a Transonic Fan Blade Through Al-Enabled Active Subspaces 2021 Lopez, Diego I.
GT2021-59495 Fan Stability With Leading Edge Damage: Blind Predietion and Validation 2021 Gunn, E. J.
GT2021-59968 Accounting for Circumferential Flow Nonuniformity in a Multi-Stage Axial Compressor 2021 Lou, Fangyuan
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
Alle Artikel auflisten