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Aeromechanical Response of a Distortion-Tolerant Boundary Layer Ingesting Fan
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.2514/6.2007-450openalex-snapshot
Performance of a Boundary Layer Ingesting (BLI) Propulsion System
inferredcites →https://doi.org/10.2514/6.2009-931openalex-snapshot
Hybrid Wing Body Configuration System Studies
inferredcites →https://doi.org/10.2514/6.2012-3995openalex-snapshot
Aeromechanics Analysis of a Boundary Layer Ingesting Fan
inferredcites →https://doi.org/10.2514/6.2014-3734openalex-snapshot
Forced Response Analysis of a Fan with Boundary Layer Inlet Distortion
inferredcites →https://doi.org/10.2514/6.2017-5041openalex-snapshot
Experimental Evaluation of an Embedded Boundary Layer Ingesting Propulsor for Highly Efficient Subsonic Cruise Aircraft
inferredcites →https://doi.org/10.2514/6.2017-5042openalex-snapshot
Design of a Distortion-Tolerant Fan for a Boundary-Layer Ingesting Embedded Engine Application
inferredcites →https://doi.org/10.2514/6.2018-1888openalex-snapshot
Data Analysis Techniques for Fan Performance in Highly-Distorted Flows from Boundary Layer Ingesting Inlets
inferredcites →https://doi.org/10.2514/6.2018-1890openalex-snapshot
Cyclic Symmetry Finite Element Forced Response Analysis of a Distortion Tolerant Fan with Boundary Layer Ingestion
inferredcites →https://doi.org/10.2514/6.2018-1891openalex-snapshot
Aeromechanics Analysis of a Distortion-Tolerant Fan with Boundary Layer Ingestion
inferredcites →https://doi.org/10.2514/6.2018-1892openalex-snapshot
Laser Displacement Measurements of Fan Blades in Resonance and Flutter During the Boundary Layer Ingesting Inlet and Distortion-Tolerant Fan Test
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/10.1016/j.ast.2021.106802openalex-snapshot
Numerical investigation on the forced vibration induced by the low engine order under boundary layer ingestion condition
inferred← citeshttps://doi.org/10.1016/j.ast.2022.107826openalex-snapshot
Aerodynamics of a short intake in crosswind
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.ast.2025.109953openalex-snapshot
Investigation of aeroelastic instability in a transonic compressor with low engine order distortion
inferred← citeshttps://doi.org/10.1016/j.ast.2026.111642openalex-snapshot
Aerodynamic performance in a boundary layer ingesting fan with swirl distortion
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2021.103412openalex-snapshot
A spatial–temporal analysis approach for flutter predictions using decoupled and fully-coupled methods
inferred← citeshttps://doi.org/10.1016/j.jweia.2022.105065openalex-snapshot
An automatized methodology to generate velocity distortion panels for wind tunnel testing
inferred← citeshttps://doi.org/10.1016/j.paerosci.2022.100810openalex-snapshot
Non-intrusive flow diagnostics for unsteady inlet flow distortion measurements in novel aircraft architectures
inferred← citeshttps://doi.org/10.1016/j.ress.2025.111192openalex-snapshot
High-cycle fatigue life prediction for fan blades considering aleatory and epistemic uncertainty with random damage
inferred← citeshttps://doi.org/10.1017/flo.2026.10052openalex-snapshot
Unsteady loss mechanisms in a boundary layer ingestion fan under inlet distortion
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/10.1115/1.4050364openalex-snapshot
Efficient Steady and Unsteady Flow Modeling for Arbitrarily Mis-Staggered Bladerow Under Influence of Inlet Distortion
inferred← citeshttps://doi.org/10.1115/1.4054035openalex-snapshot
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation
inferred← citeshttps://doi.org/10.1115/1.4063867openalex-snapshot
Aeroacoustic Effects on the Forcing of Fan and Compressor Blades Due to Distortion
inferred← citeshttps://doi.org/10.1115/1.4065517openalex-snapshot
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan
inferred← citeshttps://doi.org/10.1115/1.4066915openalex-snapshot
Fan Non-Synchronous Forced Vibration Under Crosswind
inferred← citeshttps://doi.org/10.1115/1.4070233openalex-snapshot
Impact of Fan Aerodynamics on Inlet Distortion at Crosswind
inferred← citeshttps://doi.org/10.1115/1.4072203openalex-snapshot
Mitigation of Circumferential Inlet Distortion Effects Using Non-Axisymmetric Fan Inlet and Exit Guide Vanes
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/10.1177/09544100221101669openalex-snapshot
S-duct flow distortion with non-uniform inlet conditions
inferred← citeshttps://doi.org/10.1177/09544100231153910openalex-snapshot
Conceptual aero-structural design of a fan stage under distorted flow
inferred← citeshttps://doi.org/10.1515/tjj-2025-0134openalex-snapshot
Investigation of fluid-induced vibration caused by low engine order total pressure distortions
inferred← citeshttps://doi.org/10.2514/1.b37554openalex-snapshot
Influence of Upstream Total Pressure Profiles on S-Duct Intake Flow Distortion
inferred← citeshttps://doi.org/10.2514/1.b38127openalex-snapshot
Novel Method for Evaluating Intake Unsteady Flow Distortion
inferred← citeshttps://doi.org/10.2514/1.b38231openalex-snapshot
Effect of Incoming Boundary-Layer Characteristics on Performance of a Distributed Propulsion System
inferred← citeshttps://doi.org/10.2514/6.2019-4201openalex-snapshot
An assessment on the unsteady flow distortion generated by an S-duct intake
inferred← citeshttps://doi.org/10.2514/6.2019-4202openalex-snapshot
The impact of inlet boundary layer thickness on the unsteady aerodynamics of S-duct intakes
inferred← citeshttps://doi.org/10.2514/6.2023-0502openalex-snapshot
Characterization of unsteady distortion events for S-duct intakes under non-uniform inlet conditions
inferred← citeshttps://doi.org/10.2514/6.2024-1524openalex-snapshot
Experimental Characterization of an Electric Ducted Fan for the SUSAN 25% Scale Research Vehicle
inferred← citeshttps://doi.org/10.33737/gpps23-tc-090openalex-snapshot
Effects of inlet distortion on aeroelastic stability of a transonic fan
inferred← citeshttps://doi.org/10.3390/aerospace8010016openalex-snapshot
Proof of Concept Study for Fuselage Boundary Layer Ingesting Propulsion
inferred← citeshttps://doi.org/10.70675/ef356ddez33c2z4d00z926cz6799ed2fc2c0openalex-snapshot
Fan blade flutter prediction with nonlinear contact interfaces at blade roots
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