Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition June 7-11, 2021, virtual, online Volume 2 Turbomachinery A Axial flow fan and compressor aerodynamics

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Bibliographische Detailangaben
Körperschaften:	ASME Turbo Expo (VerfasserIn), International Gas Turbine Institute (SponsorIn), American Society of Mechanical Engineers (Herausgebendes Organ)
Format:	UnknownFormat
Sprache:	eng
Veröffentlicht:	New York, N.Y. The American Society of Mechanical Engineers 2021
Schlagworte:	Konferenzschrift
Online Zugang:	Inhaltsverzeichnis
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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
GT2021-01098 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
GT2021-59926 Application of a Viscous Through-Flow Model to a Modern Axial Low-Pressure Compressor	2021	Budo, Arnaud
GT2021-60314 Effect of the Axial Casing Groove Geometry on the Production and Distribution of Reynolds Stresses in the Tip Region of an Axial Compressor Rotor	2021	Koley, Subhra Shankha
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

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