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Surface flow and vortex shedding of an impulsively started wing

https://doi.org/10.1017/s002211200100489x
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inferred← citeshttps://doi.org/10.2139/ssrn.4518066openalex-extracted
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inferred← citeshttps://doi.org/10.1007/s00348-007-0428-6openalex-snapshot
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inferred← citeshttps://doi.org/10.1007/s00348-009-0713-7openalex-snapshot
The ultra-low Reynolds number airfoil wake
inferred← citeshttps://doi.org/10.1007/s00348-010-1038-2openalex-snapshot
Scale-up of an unsteady flow field for enhanced spatial and temporal resolution of PIV measurements: application to leaflet wake flow in a mechanical heart valve
inferred← citeshttps://doi.org/10.1007/s00348-012-1270-zopenalex-snapshot
Parametric study of separation and transition characteristics over an airfoil at low Reynolds numbers
inferred← citeshttps://doi.org/10.1007/s00348-014-1699-3openalex-snapshot
Bayesian inference applied to spatio-temporal reconstruction of flows around a NACA0012 airfoil
inferred← citeshttps://doi.org/10.1007/s00348-016-2165-1openalex-snapshot
Dynamic mode decomposition for non-uniformly sampled data
inferred← citeshttps://doi.org/10.1007/s00348-017-2455-2openalex-snapshot
Time-resolved flow reconstruction with indirect measurements using regression models and Kalman-filtered POD ROM
inferred← citeshttps://doi.org/10.1016/j.ast.2008.05.001openalex-snapshot
Frequency effects on the aerodynamic mechanisms of a heaving airfoil in a forward flight configuration
inferred← citeshttps://doi.org/10.1016/j.ast.2010.10.005openalex-snapshot
Reynolds number effects on flow characteristics and aerodynamic performances of a swept-back wing
inferred← citeshttps://doi.org/10.1016/j.ast.2020.106056openalex-snapshot
POD analysis of the unsteady behavior of blade wake under the influence of laminar separation vortex shedding in a compressor cascade
inferred← citeshttps://doi.org/10.1016/j.compfluid.2018.02.014openalex-snapshot
Fluid flow around NACA 0012 airfoil at low-Reynolds numbers with hybrid lattice Boltzmann method
inferred← citeshttps://doi.org/10.1016/j.energy.2017.12.045openalex-snapshot
Identification of flow phenomena over NACA 4412 wind turbine airfoil at low Reynolds numbers and role of laminar separation bubble on flow evolution
inferred← citeshttps://doi.org/10.1016/j.energy.2026.141229openalex-snapshot
An energy loss evaluation of vortex evolution mechanisms and entropy production coupling in a low-head mixed-flow PAT system based on a time-lagged lasso regression model
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2010.01.011openalex-snapshot
Computational and experimental investigations of performance curve of an axial flow fan using downstream flow resistance method
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2015.09.031openalex-snapshot
A stratified wake of a hydrofoil accelerating from rest
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2020.110296openalex-snapshot
Control of the flow in the near wake of an airfoil at full stall using fixed trailing-edge plates
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2022.110622openalex-snapshot
Turbulent structures in an airfoil wake at ultra-low to low Reynolds numbers
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2021.108920openalex-snapshot
Hysteresis of two-dimensional flows around a NACA0012 airfoil at Re=5000 and linear analyses of their mean flow.
inferred← citeshttps://doi.org/10.1016/j.jcp.2023.112630openalex-snapshot
BiGlobal stability analysis for flow in complex geometry based on immersed boundary method
inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2016.01.003openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2016.03.012openalex-snapshot
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inferred← citeshttps://doi.org/10.1016/j.jfluidstructs.2025.104296openalex-snapshot
Experimental investigation on fluid–structure interaction in highly flexible wings
inferred← citeshttps://doi.org/10.1016/j.oceaneng.2021.108889openalex-snapshot
Design of wind-turbine blades for improving aerodynamic performance using hybrid blades
inferred← citeshttps://doi.org/10.1016/j.paerosci.2020.100616openalex-snapshot
Current status of Lattice Boltzmann Methods applied to aerodynamic, aeroacoustic, and thermal flows
inferred← citeshttps://doi.org/10.1017/jfm.2016.778openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2018.189openalex-snapshot
Multiple bifurcations of the flow over stalled airfoils when changing the Reynolds number
inferred← citeshttps://doi.org/10.1017/jfm.2020.248openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2022.612openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2022.958openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2023.41openalex-snapshot
Global stability, sensitivity and passive control of low-Reynolds-number flows around NACA 4412 swept wings
inferred← citeshttps://doi.org/10.1017/jfm.2023.890openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2025.10470openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/jfm.2026.11425openalex-snapshot
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inferred← citeshttps://doi.org/10.1017/s0022112009007058openalex-snapshot
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inferred← citeshttps://doi.org/10.1038/nature02000openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/1.2187069openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/1.5003578openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/1.5085250openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/5.0138396openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/5.0174145openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/5.0196040openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/5.0246708openalex-snapshot
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inferred← citeshttps://doi.org/10.1063/5.0261509openalex-snapshot
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inferred← citeshttps://doi.org/10.1080/02533839.2003.9670755openalex-snapshot
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inferred← citeshttps://doi.org/10.1088/0960-1317/17/10/021openalex-snapshot
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inferred← citeshttps://doi.org/10.1088/1748-3190/ac98e5openalex-snapshot
Capturing wake capture: a 2D numerical investigation into wing–wake interaction aerodynamics
inferred← citeshttps://doi.org/10.1098/rsta.2010.0355openalex-snapshot
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inferred← citeshttps://doi.org/10.1103/physreve.99.043110openalex-snapshot
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inferred← citeshttps://doi.org/10.1108/hff-10-2016-0391openalex-snapshot
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inferred← citeshttps://doi.org/10.1109/mepe64515.2024.11115296openalex-snapshot
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inferred← citeshttps://doi.org/10.1115/1.2776964openalex-snapshot
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inferred← citeshttps://doi.org/10.1177/1756829316653700openalex-snapshot
On the wake pattern of symmetric airfoils for different incidence angles at Re = 1000
inferred← citeshttps://doi.org/10.1177/17568293211055653openalex-snapshot
Vortex flow aerodynamics behind a symmetric airfoil at low angles of attack and Reynolds numbers
inferred← citeshttps://doi.org/10.1177/17568293211055656openalex-snapshot
Direct Numerical Simulations on the three-dimensional wake transition of flows over NACA0012 airfoil at Re = 1000
inferred← citeshttps://doi.org/10.1242/jeb.01262openalex-snapshot
Dragonfly flight: free-flight and tethered flow visualizations reveal a diverse array of unsteady lift-generating mechanisms, controlled primarilyviaangle of attack
inferred← citeshttps://doi.org/10.1260/1756-8293.7.3.301openalex-snapshot
On the Unsteady Behavior of the Flow around NACA 0012 Airfoil with Steady External Conditions at Re=1000
inferred← citeshttps://doi.org/10.20868/upm.thesis.43089openalex-snapshot
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inferred← citeshttps://doi.org/10.2139/ssrn.4806241openalex-snapshot
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inferred← citeshttps://doi.org/10.2139/ssrn.4811644openalex-snapshot
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inferred← citeshttps://doi.org/10.2322/astj.23.18openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.24045openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.24517openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j051028openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j053764openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j054138openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j056774openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j064345openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/1.j066220openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2003-230openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2004-2345openalex-snapshot
U-ZEN: A Computational Tool Solving U-Rans Equations for Industrial Unsteady Applications
inferred← citeshttps://doi.org/10.2514/6.2008-3957openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2010-1043openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2010-4628openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2017-0997openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2022-0467openalex-snapshot
Experimental Investigation on the Effect of Sweep and Taper on Low Reynolds Number Finite Wings
inferred← citeshttps://doi.org/10.2514/6.2022-2428openalex-snapshot
From biglobal to triglobal resolvent analysis: laminar separated flows over swept wings
inferred← citeshttps://doi.org/10.2514/6.2023-0077openalex-snapshot
Resolvent-based estimation of flow around an airfoil for closed-loop control
inferred← citeshttps://doi.org/10.2514/6.2023-2297openalex-snapshot
Wake dynamics of tapered wings. Part I: a computational study
inferred← citeshttps://doi.org/10.2514/6.2023-2298openalex-snapshot
Wake dynamics of tapered wings. Part II: an experimental study
inferred← citeshttps://doi.org/10.2514/6.2024-1355openalex-snapshot
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inferred← citeshttps://doi.org/10.2514/6.2025-1828openalex-snapshot
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inferred← citeshttps://doi.org/10.32657/10356/6136openalex-snapshot
Two-stream mixing flow with streamwise vorticity
inferred← citeshttps://doi.org/10.3390/math13101671openalex-snapshot
Finite Volume Incompressible Lattice Boltzmann Framework for Non-Newtonian Flow Simulations in Complex Geometries
inferred← citeshttps://doi.org/10.3934/mina.2024015openalex-snapshot
A two- to three-dimensional wake transition mechanism induced by the angle of attack of a NACA0012 airfoil
inferred← citeshttps://doi.org/10.47176/jafm.15.03.33099openalex-snapshot
Critical Angle and Fundamental Frequency of Symmetric Airfoils at Low Reynolds Numbers
inferred← citeshttps://doi.org/10.70675/c7af5454zbd99z4da9zbf4azdf9ed88e1e27openalex-snapshot
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