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Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing

https://doi.org/10.1115/1.3239730
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inferred← citeshttps://doi.org/10.1115/97-gt-406openalex-snapshot
Effects of Non-Axisymmetric Tip Clearance on Axial Compressor Performance and Stability
inferred← citeshttps://doi.org/10.1115/97-gt-415openalex-snapshot
Viscous Throughflow Modelling of Axial Compressor Bladerows Using a Tangential Blade Force Hypothesis
inferred← citeshttps://doi.org/10.1115/98-gt-334openalex-snapshot
Experimental Evaluation of the High-to-Low Speed Transformation Process for a Highly Loaded Core Compressor Stage
inferred← citeshttps://doi.org/10.1115/99-gt-210openalex-snapshot
Aerodynamic Design and Testing of an Axial Flow Compressor With Pressure Ratio of 23.3:1 for the LM2500+ Gas Turbine
inferred← citeshttps://doi.org/10.1115/gt2002-30358openalex-snapshot
Effect of Upstream Unsteady Flow Conditions on Rotor Tip Leakage Flow
inferred← citeshttps://doi.org/10.1115/gt2004-53012openalex-snapshot
Design and Test of an Ultra-Low Solidity Flow-Controlled Compressor Stator
inferred← citeshttps://doi.org/10.1115/gt2015-42121openalex-snapshot
Aerodynamic Investigation of a Single-Stage Axial Compressor With a Casing Groove and Tip Injection Using Fluid-Structure Interaction Analysis
inferred← citeshttps://doi.org/10.1115/gt2016-56232openalex-snapshot
Influence of Tip Clearance on the Performance and Matching of Multistage Axial Compressors
inferred← citeshttps://doi.org/10.1115/gt2016-57163openalex-snapshot
Measurements and Modelling of Ingress in a New 1.5-Stage Turbine Research Facility
inferred← citeshttps://doi.org/10.1115/gt2016-57396openalex-snapshot
Design of Compressor Endwall Velocity Triangles
inferred← citeshttps://doi.org/10.1115/gt2016-57727openalex-snapshot
Effects of Rotor Tip Blade Loading Variation on Compressor Stage Performance
inferred← citeshttps://doi.org/10.1115/gt2017-63051openalex-snapshot
Experimental and Numerical Investigation of a Circumferential Groove Casing Treatment in a Low Speed Axial Research Compressor at Different Tip Clearances
inferred← citeshttps://doi.org/10.1115/gt2017-64422openalex-snapshot
On Scaling Method to Investigate High-Speed Over-Tip-Leakage Flow at Low-Speed Condition
inferred← citeshttps://doi.org/10.1115/gt2018-77016openalex-snapshot
The Comparison of Aerodynamic Performance Data Acquired From Thermal Measurements and a Torquemeter on a Compressor Impeller
inferred← citeshttps://doi.org/10.1115/gt2020-15209openalex-snapshot
Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations
inferred← citeshttps://doi.org/10.1115/gt2020-15940openalex-snapshot
Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator
inferred← citeshttps://doi.org/10.1115/gt2021-58946openalex-snapshot
Design and Pre-Test Evaluation of a Low-Pressure Compressor Test Facility for Cryogenic Hydrogen Fuel Integration
inferred← citeshttps://doi.org/10.1115/gtindia2017-4880openalex-snapshot
Design Aspects for Large Diameter, Low Speed Axial Flow Fan for Wind Tunnel Application
inferred← citeshttps://doi.org/10.1115/imece2015-52293openalex-snapshot
Effect of a New Vortex Generator on the Performance of an Axial Compressor Cascade at Design and Off-Design Conditions
inferred← citeshttps://doi.org/10.1117/12.3005939openalex-snapshot
Design and performance analysis of tetrafurcated fiber optic displacement sensors for enhanced range and linearity
inferred← citeshttps://doi.org/10.1117/12.3022354openalex-snapshot
Optical fiber sensors for simultaneous measurement of angular and linear displacement
inferred← citeshttps://doi.org/10.1155/2015/146272openalex-snapshot
Experimental Investigation of Factors Influencing Operating Rotor Tip Clearance in Multistage Compressors
inferred← citeshttps://doi.org/10.1155/2017/4631751openalex-snapshot
Investigation of Performance and Rotor Tip Flow Field in a Low Speed Research Compressor with Circumferential Groove Casing Treatment at Varying Tip Clearance
inferred← citeshttps://doi.org/10.1177/0020294019877514openalex-snapshot
A review of blade tip clearance–measuring technologies for gas turbine engines
inferred← citeshttps://doi.org/10.1177/0954410014537803openalex-snapshot
Effects of low Reynolds number on flow stability of a transonic compressor
inferred← citeshttps://doi.org/10.1177/0954410015621928openalex-snapshot
The effect of end wall boundary layer on matching and corresponding flow control technique for multistage axial compressor
inferred← citeshttps://doi.org/10.1177/0954410017734884openalex-snapshot
Investigation of endwall treatment and shock control in a five-stage axial compressor
inferred← citeshttps://doi.org/10.1177/0954410019897467openalex-snapshot
Effect of tip clearance dimension on unsteadiness in a low-reaction aspirated transonic compressor rotor
inferred← citeshttps://doi.org/10.1177/0957650914560451openalex-snapshot
Investigation of the internal flow field for a subsonic stage of high pressure compressor through model testing
inferred← citeshttps://doi.org/10.1177/1687814016674629openalex-snapshot
Research on three-dimensional blade designs in an ultra-highly loaded low-speed axial compressor stage: Design and numerical investigations
inferred← citeshttps://doi.org/10.1243/0954406991522220openalex-snapshot
The exploitation of three-dimensional flow in turbomachinery design
inferred← citeshttps://doi.org/10.1243/0954406991522680openalex-snapshot
Axial flow compressor design †
inferred← citeshttps://doi.org/10.1243/095765005x28607openalex-snapshot
Performance enhancement in transonic axial compressors using blade tip injection coupled with casing treatment
inferred← citeshttps://doi.org/10.1515/tjj-2016-0077openalex-snapshot
Effects of Non-axisymmetric Casing Grooves Combined with Airflow Injection on Stability Enhancement of an Axial Compressor
inferred← citeshttps://doi.org/10.1515/tjj-2022-0054openalex-snapshot
Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors
inferred← citeshttps://doi.org/10.1515/tjj.1996.13.3.155openalex-snapshot
Design, Development, and Performance of a Turbine Research Facility to Study Rotor Stator Interaction Effects
inferred← citeshttps://doi.org/10.2139/ssrn.5634428openalex-snapshot
The Suppression Effect of a Circumferentially Expanding Clearance Structure on Leakage Flow in a Transonic Rotor under Variable Rotational Speed Conditions
inferred← citeshttps://doi.org/10.21595/jve.2017.17863openalex-snapshot
Effect of counter-rotating fan’s speed matching on stall inception and characteristics of tip clearance flow
inferred← citeshttps://doi.org/10.21608/asat.2009.23850openalex-snapshot
High Speed Inlet Stage for an Advanced High-Pressure Ratio Core Compressor: Numerical Flow Field Prediction and Verification
inferred← citeshttps://doi.org/10.2514/1.25530openalex-snapshot
Characteristics of the Tip Leakage Vortex in a Low-Speed Axial Compressor
inferred← citeshttps://doi.org/10.2514/1.2703openalex-snapshot
Three-Dimensional Multi-Objective Design Optimization of a Transonic Compressor Rotor
inferred← citeshttps://doi.org/10.2514/1.54930openalex-snapshot
Streamwise Evolution of Loss in a Shrouded Axial Compressor Cascade Passage
inferred← citeshttps://doi.org/10.2514/1.b34599openalex-snapshot
Tip Flow Unsteadiness and Blade Row Interactions for a Low-Speed Compressor Rotor
inferred← citeshttps://doi.org/10.2514/1.b35981openalex-snapshot
Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage
inferred← citeshttps://doi.org/10.2514/1.b36617openalex-snapshot
Effect of Nonuniform Tip Clearance on the Performance of Transonic Axial Compressors
inferred← citeshttps://doi.org/10.2514/3.23044openalex-snapshot
Experimental study of end-wall flow in a compressor cascade
inferred← citeshttps://doi.org/10.2514/3.23178openalex-snapshot
Improved compressor performance using recessed clearance (trenches)
inferred← citeshttps://doi.org/10.2514/6.1985-174openalex-snapshot
Three dimensional aerodynamics of an annular cascade in a non-uniform inlet flow
inferred← citeshttps://doi.org/10.2514/6.1986-1745openalex-snapshot
Improved compressor performance using recessed clearance (trenches) over the rotor
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