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Distortion-Induced Vibration in Fan and Compressor Blading

https://doi.org/10.2514/3.59819
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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/0022-460x(66)90102-7openalex-snapshot
Some intake flow maldistribution effects on compressor rotor blade vibration
inferredcites →https://doi.org/10.1115/1.3423070openalex-snapshot
The Unsteady Aerodynamics of a Finite Supersonic Cascade With Subsonic Axial Flow
inferredcites →https://doi.org/10.1115/1.3616710openalex-snapshot
Recent Blade Vibration Techniques
inferredcites →https://doi.org/10.2514/6.1967-18openalex-snapshot
The unsteady normal force response of an airfoil in a periodically distorted inlet flow including stalling effects
inferredcites →https://doi.org/10.2514/6.1969-485openalex-snapshot
Attenuation of inlet flow distortion upstream of axial flow compressors

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/10.1007/978-94-009-5153-2_23openalex-snapshot
Organization of Design Systems for Turbomachinery
inferred← citeshttps://doi.org/10.1016/0376-0421(76)90004-xopenalex-snapshot
Reliability of compressor aerofoils
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.jsv.2021.116628openalex-snapshot
Identification of the excitation source's circumferential position for rotating blades based on vibration phase
inferred← citeshttps://doi.org/10.1115/1.4048965openalex-snapshot
Design Space Exploration of Rotor Blades Accounting for Vibratory Responses by Indirect Emulation
inferred← citeshttps://doi.org/10.2514/1.46046openalex-snapshot
Numerical Investigation of Inlet Distortion on a Wing-Embedded Lift Fan
inferred← citeshttps://doi.org/10.2514/3.44452openalex-snapshot
Blade vibration - Some key elements in design verification
inferred← citeshttps://doi.org/10.2514/5.9781624107221.0895.0974openalex-snapshot
Aeromechanics
inferred← citeshttps://doi.org/10.2514/6.1997-3364openalex-snapshot
Inlet distortion considerations for high cycle fatigue in gas turbine engine
inferred← citeshttps://doi.org/10.2514/6.2009-865openalex-snapshot
Numerical Researches on Aeroelastic Problem of a Rotor due to IGV/Fan Interaction
inferred← citeshttps://doi.org/10.2514/6.2013-2409openalex-snapshot
Forced Response Analysis of Compressor Blades under Unsteady Inlet Distortion
inferred← citeshttps://doi.org/10.33737/gpps23-tc-090openalex-snapshot
Effects of inlet distortion on aeroelastic stability of a transonic fan
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