GT2022-82075 Flow Dynamics of a Subsonic Axial Compressor Rotor With Leaned Tandem Blades

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:ASME Turbo Expo (67. : 2022 : Rotterdam) Proceedings of ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition (GT 2022) ; Volume 10, A: Turbomachinery: Axial flow fan and compressor aerodynamics
1. Verfasser: Kumar, Amit (VerfasserIn)
Weitere Verfasser: John, Jerry T. (VerfasserIn), Kumar, Akshay (VerfasserIn), Chhugani, Hitesh (VerfasserIn), Pradeep, A. M. (VerfasserIn)
Pages:2022
Format: UnknownFormat
Sprache:eng
Veröffentlicht: 2022
Schlagworte:
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Titel Jahr Verfasser
GT2022-80083 Effects of Bleed Slot Size on the Shock-Wave/Boundary-Layer Interactions in a Transonic Compressor Stator 2022 Li, Bai
GT2022-80538 Large Eddy Simulation of an Open Rotor Fan Blade 2022 Priebe, Stephan
GT2022-81016 Attributes of Bi-Directional Turbomachinery for Pumped Thermal Energy Storage 2022 Chiapper, J. D.
GT2022-81678 Investigation of the Impact of Realistic Inlet Distortions on a 1.5-Stage Transonic Compressor 2022 Werner, Jan
GT2022-82143 Numerical Investigation of Near-Tip Modifications for a Highly-Loaded Low-Speed Rotor Under the Influence of Double Leakage 2022 Eckel, Jannik
GT2022-82177 Effects of Sideslip Direction on a Rear Fuselage Boundary Layer Ingesting Fan 2022 Pardo, Alejandro Castillo
GT2022-82242 Impact of Operating Conditions and Axial Casing Grooves on the Evolution of Flow Structure Across Blade Rows in an Axial Compressor 2022 Saraswat, Ayush
GT2022-82834 Numerical Investigations on the Rotating Stall in an Axial Compressor and Its Control by Flow Injection at Casing 2022 Marty, Julien
GT2022-83363 Stall Margin Improvement in a Transonic Compressor With a Casing Treatment: Flow Mechanism 2022 Hah, Chunill
GT2022-83452 Experimental Investigation of Inlet Stagnation Pressure Distortion Effects on a Transonic Axial Compressor Rotor 2022 Oliva, Andrew A.
GT2022-83551 Effects of Pure Shearing and Rigid-Body Rotation on the Evolution of Tip Leakage Vortex in an Axial Compressor Rotor 2022 Liu, Yangwei
GT2022-83599 Compressor Maps and Coupling: Symmetry, Geometry, and Universility 2022 Iwrey, Benjamin
GT2022-77977 Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor 2022 Seki, Ryosuke
GT2022-78443 Numerical Analysis of Blade Platform Leakage in Axial Compressors 2022 Petermann, Jannik
GT2022-79522 The Modelling of Roughness Effect on the Performance of a Controlled Diffusion Airfoll 2022 Delvaux, Gregory
GT2022-80284 PDA Laser Measurements of Droplet-Laden Flows in a Four Stage Axial Compressor 2022 Doerr, Tobias
GT2022-80914 Effect of the Axial Compressor Tip Clearance Size: Performance and Transition to Rotating Stall 2022 Rannou, Clemence
GT2022-82258 Evolution of Turbulence and Its Modification by Axial Casing Grooves in a Multi-Stage Axial Compressor 2022 Koley, Subhra Shankha
GT2022-82465 Mitigation of BLI Circumferential Distortion Using Non-Axisymmetric Fan Exit Guide Vanes 2022 Hall, David
GT2022-82720 Insights Into the Unsteady Shock Boundary Layer Interaction 2022 Hergt, A.
Alle Artikel auflisten