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Attenuation of circumferential inlet distortion in multistage axial compressors.
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.2514/8.3870openalex-snapshot
Circumferential Inlet Distortions in Axial Flow Turbomachinery
inferredcites →https://doi.org/10.2514/8.8286openalex-snapshot
An Actuator Disc Analysis of Inlet Distortion and Rotating Stall in Axial Flow Turbomachines
inferredcites →https://doi.org/10.7907/5214-1s06.openalex-snapshot
Performance of Axial Compressors with Asymmetric Inlet Flows
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.2139/ssrn.4855614openalex-extracted
Design and Aerodynamic Stability Improvement Study of Non-Axisymmetric Stator Fan Under Distorted Insertion Plate Configuration
inferred← citeshttps://doi.org/10.1007/978-3-540-72412-4_1openalex-snapshot
Study on the Propagation of Inlet Flow Distortion in Axial Compressor Using an Integral Method
inferred← citeshttps://doi.org/10.1007/978-3-540-72412-4_4openalex-snapshot
A Development of Novel Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor
inferred← citeshttps://doi.org/10.1016/0167-6105(93)90270-xopenalex-snapshot
Numerical simulation of the flow field near an axial flow fan operating under distorted inflow conditions
inferred← citeshttps://doi.org/10.1016/j.ast.2020.106433openalex-snapshot
Stall inception prediction of axial compressors with radial inlet distortions
inferred← citeshttps://doi.org/10.1016/j.ast.2024.109537openalex-snapshot
Design and aerodynamic stability improvement study of a non-axisymmetric stator fan in a distorted insertion plate configuration
inferred← citeshttps://doi.org/10.1016/j.cja.2016.10.023openalex-snapshot
Influence of SPS casing treatment on axial flow compressor subjected to radial pressure distortion
inferred← citeshttps://doi.org/10.1017/s0001924000041610openalex-snapshot
Some aspects of inlet/engine flow compatibility
inferred← citeshttps://doi.org/10.1115/1.0002787vopenalex-snapshot
Efficient Steady and Unsteady Flow Modeling for Arbitrarily Mis-Staggered Bladerow Under Influence of Inlet Distortion
inferred← citeshttps://doi.org/10.1115/1.3148478openalex-snapshot
High-Fidelity Numerical Analysis of Per-Rev-Type Inlet Distortion Transfer in Multistage Fans—Part I: Simulations With Selected Blade Rows
inferred← citeshttps://doi.org/10.1115/1.4003850openalex-snapshot
A Study of Fan-Distortion Interaction Within the NASA Rotor 67 Transonic Stage
inferred← citeshttps://doi.org/10.1115/1.4025953openalex-snapshot
Influence of Circumferential Inflow Distortion on the Performance of a Low Speed, High Aspect Ratio Contra Rotating Axial Fan
inferred← citeshttps://doi.org/10.1115/1.4050364openalex-snapshot
Efficient Steady and Unsteady Flow Modeling for Arbitrarily Mis-Staggered Bladerow Under Influence of Inlet Distortion
inferred← citeshttps://doi.org/10.1115/gt2014-26666openalex-snapshot
Effect of BLI–Type Inlet Distortion on Turbofan Engine Performance
inferred← citeshttps://doi.org/10.1115/gt2020-16204openalex-snapshot
Efficient Steady and Unsteady Flow Modeling for Arbitrarily Mis-Staggered Bladerow Under Influence of Inlet Distortion
inferred← citeshttps://doi.org/10.1155/2011/182906openalex-snapshot
Development of a Method for Enhanced Fan Representation in Gas Turbine Modeling
inferred← citeshttps://doi.org/10.1155/ijrm.2005.117openalex-snapshot
An Improved Integral Method for Predictionof Distorted Inlet Flow Propagation in Axial Compressor
inferred← citeshttps://doi.org/10.1243/jmes_jour_1976_018_007_02openalex-snapshot
Compressor-Diffuser Interaction with Circumferential Flow Distortion
inferred← citeshttps://doi.org/10.2514/1.c031789openalex-snapshot
Computational Investigation of Inlet Distortion at High Angles of Attack
inferred← citeshttps://doi.org/10.2514/2.5253openalex-snapshot
Influence of Inlet Pressure Distortion on a Convertible Engine Fan
inferred← citeshttps://doi.org/10.2514/3.44259openalex-snapshot
Attenuation of inlet flow distortion upstream of axial flow compressors
inferred← citeshttps://doi.org/10.2514/3.44589openalex-snapshot
Coupled compressor-diffuser flow instability
inferred← citeshttps://doi.org/10.2514/3.57927openalex-snapshot
Combined Pressure and Temperature Distortion Effects on Internal Flow of a Turbofan Engine
inferred← citeshttps://doi.org/10.2514/3.9227openalex-snapshot
Nonaxisymmetric compressible swirling flow in turbomachine annuli
inferred← citeshttps://doi.org/10.2514/6.1968-565openalex-snapshot
Insights into axial compressor response to distortion
inferred← citeshttps://doi.org/10.2514/6.2013-3602openalex-snapshot
The Influence of Duct Development Distance on Screen-Generated Total Pressure Distortion Profiles
inferred← citeshttps://doi.org/10.33737/gpps21-tc-287openalex-snapshot
Experimental Investigation Of Circumferential Inlet Distortion On Partial Surge Type Stall Inception In A Transonic Axial Compressor
inferred← citeshttps://doi.org/10.5772/54411openalex-snapshot
Synthesis of Flow Simulation Methods for Fast and Accurate Gas Turbine Engine Performance Estimation
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