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Dynamic stall simulation of a pitching airfoil under unsteady freestream velocity
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1 of the 40 references listed on this page is in the Retraction Watch database as retracted (export 2026-10-28): 10.1109/iccet.2010.5486034 (notice 2010-06-17).
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1007/bf00193856openalex-snapshotInvestigation of the unsteady flow velocity field above an airfoil pitching under deep dynamic stall conditions
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.4529476openalex-extractedAeroacoustics Simulation of a Dynamic Wind Turbine Blade Section Under Yaw Loads for Estimation of Noise Pollution
inferred← citeshttps://doi.org/10.1002/ese3.1896openalex-snapshotNumerical study of dynamic stall effects on VR‐12 airfoil with pitch oscillation and accelerated inflow
inferred← citeshttps://doi.org/10.1007/s10973-019-08402-6openalex-snapshotA numerical investigation on the heat transfer characteristics of nanofluid flow in a three-dimensional microchannel with harmonic rotating vortex generators
inferred← citeshttps://doi.org/10.1007/s13369-023-07892-9openalex-snapshotOptimization of Blowing Jet Performance on Wind Turbine Airfoil Under Dynamic Stall Conditions Using Active Machine Learning and Computational Intelligence
inferred← citeshttps://doi.org/10.1016/j.rineng.2019.100037openalex-snapshotEvaluating the influence of unsteady air density to the aerodynamic performance of a fixed wing aircraft at different angle of attack using computational fluid dynamics
inferred← citeshttps://doi.org/10.1016/j.seta.2020.100748openalex-snapshotComputational evaluation of an optimum leading-edge slat deflection angle for dynamic stall control in a novel urban-scale vertical axis wind turbine for low wind speed operation
inferred← citeshttps://doi.org/10.1061/jaeeez.aseng-5429openalex-snapshotDynamic Stall Alleviation of a Helicopter Blade Section in Forward Flight Condition Using an Optimized Combination of Active Nose Droop and Active Gurney Flap
inferred← citeshttps://doi.org/10.1063/1.5114833openalex-snapshotFlow mechanism for the effect of pivot point on the aerodynamic characteristics of a pitching airfoil and its manipulation
inferred← citeshttps://doi.org/10.1063/1.5128341openalex-snapshotNew method for dynamic mode decomposition of flows over moving structures based on machine learning (hybrid dynamic mode decomposition)
inferred← citeshttps://doi.org/10.1063/1.5142465openalex-snapshotNumerical investigation of control of dynamic stall over a NACA0015 airfoil using dielectric barrier discharge plasma actuators
inferred← citeshttps://doi.org/10.1063/5.0065788openalex-snapshotVortex control strategy for unsteady aerodynamic optimization of a plunging airfoil at a low Reynolds number
inferred← citeshttps://doi.org/10.1063/5.0153485openalex-snapshotNumerical investigation of the effect of dielectric barrier discharge plasma actuator-induced momentum jet parameters on flow control of an oscillating wind turbine airfoil
inferred← citeshttps://doi.org/10.1063/5.0164437openalex-snapshotMachine learning-based optimization of a pitching airfoil performance in dynamic stall conditions using a suction controller
inferred← citeshttps://doi.org/10.1063/5.0267855openalex-snapshotResponse of unsteady loads and flow structures of pitching airfoil and cycloidal propeller in a surging inflow
inferred← citeshttps://doi.org/10.1063/5.0268530openalex-snapshotEffect of surge and sway combined motion on the dynamic stall of floating offshore wind turbine airfoils
inferred← citeshttps://doi.org/10.1063/5.0281017openalex-snapshotParameter analysis of dual synthetic jets control for rotor airfoil dynamic stall under unsteady freestream
inferred← citeshttps://doi.org/10.1063/5.0333055openalex-snapshotKinematic regimes and wake topologies of a two-degree-of-freedom airfoil with distinct heave and pitch stiffnesses in flow-induced vibrations
inferred← citeshttps://doi.org/10.1063/5.0346109openalex-snapshotAerodynamic performance and vortex mechanisms of a bird-like airfoil with coupled pitching, plunging, and sweeping motions
inferred← citeshttps://doi.org/10.1115/1.4040795openalex-snapshotThe Role of Frequency and Phase Difference Between the Flow and the Actuation Signal of a Tangential Synthetic Jet on Dynamic Stall Flow Control
inferred← citeshttps://doi.org/10.1115/1.4046730openalex-snapshotCapturing the Dynamic Stall in H-Type Darrieus Wind Turbines Using Different URANS Turbulence Models
inferred← citeshttps://doi.org/10.1115/1.4070163openalex-snapshotEvaluating the Performance of an H-Type Wind Turbine: How Stalling Stages and Blade–Vortex Interactions Affect the Turbine?
inferred← citeshttps://doi.org/10.1115/gt2022-81988openalex-snapshotDirect Numerical Simulations of Aerodynamic Performance of Wind Turbine Airfoil by Considering Flap-Wise Blade Oscillations
inferred← citeshttps://doi.org/10.11395/aem.5.0_38openalex-snapshotExperimental Study on the Influence of Frequency Ratio on Thrust and Vortex Structure of a Pitching Wing in a Periodic Flow
inferred← citeshttps://doi.org/10.1177/09544100221097521openalex-snapshotUnsteady and nonlinear aerodynamic prediction of airfoil undergoing large-amplitude pitching oscillation based on gated recurrent unit network
inferred← citeshttps://doi.org/10.22215/etd/2017-12184openalex-snapshotInvestigating the Impact of Using CFD Generated Unsteady Mach Number Dynamic Stall Data for Numerical Rotor Analysis of Helicopter Forward Flight
inferred← citeshttps://doi.org/10.2514/6.2017-3052openalex-snapshotInvestigating the impact of using CFD generated unsteady Mach number dynamic stall data for numerical rotor analysis of helicopter forward flight
inferred← citeshttps://doi.org/10.3390/en11123341openalex-snapshotStochastic Dynamic Response Analysis of a 10 MW Tension Leg Platform Floating Horizontal Axis Wind Turbine
inferred← citeshttps://doi.org/10.3390/en15155625openalex-snapshotTwo-Dimensional URANS Numerical Investigation of Critical Parameters on a Pitch Oscillating VAWT Airfoil under Dynamic Stall
inferred← citeshttps://doi.org/10.4108/eai.7-12-2021.2314535openalex-snapshotNumerical and experimental investigation on the effects of bumps over the leading edge of the micro wind turbine blades suitable for low wind regimes
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