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Experimental investigation of dynamic stall for a pitching airfoil

https://doi.org/10.2514/3.45050
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inferred← citeshttps://doi.org/10.2139/ssrn.4656686openalex-extracted
Dynamic-Stall-Driven Vertical Axis Wind Turbine: An Experimental Study
inferred← citeshttps://doi.org/10.1007/978-3-030-05455-7_14-1openalex-snapshot
Aerofoil Aerodynamics of Wind Energy Devices
inferred← citeshttps://doi.org/10.1007/978-3-030-31307-4_14openalex-snapshot
Dynamic Stall
inferred← citeshttps://doi.org/10.1007/s003480050214openalex-snapshot
Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors
inferred← citeshttps://doi.org/10.1016/j.apenergy.2024.123199openalex-snapshot
Dynamic-stall-driven vertical axis wind turbine: An experimental parametric study
inferred← citeshttps://doi.org/10.1016/j.ast.2021.106706openalex-snapshot
Study on dynamics of vortices in dynamic stall of a pitching airfoil using Lagrangian coherent structures
inferred← citeshttps://doi.org/10.1016/j.jweia.2020.104264openalex-snapshot
A critical analysis of the stall onset in vertical axis wind turbines
inferred← citeshttps://doi.org/10.1016/j.oceaneng.2023.115556openalex-snapshot
Dynamic process and dynamic-stall phenomenon on blade sections of a floating horizontal-axis wind turbine caused by the platform's pitch motion
inferred← citeshttps://doi.org/10.1017/s0022112088000722openalex-snapshot
Separation and reattachment near the leading edge of a thin oscillating airfoil
inferred← citeshttps://doi.org/10.1063/5.0096622openalex-snapshot
Quantitative analysis of fluid transport in dynamic stall of a pitching airfoil using variational Lagrangian coherent structures and lobe dynamics
inferred← citeshttps://doi.org/10.1115/1.2346703openalex-snapshot
A New Stall-Onset Criterion for Low Speed Dynamic-Stall
inferred← citeshttps://doi.org/10.1242/jeb.040857openalex-snapshot
The importance of leading edge vortices under simplified flapping flight conditions at the size scale of birds
inferred← citeshttps://doi.org/10.1260/175682909789996186openalex-snapshot
High-Amplitude Pitch of a Flat Plate: An Abstraction of Perching and Flapping
inferred← citeshttps://doi.org/10.2514/1.j055244openalex-snapshot
Effects of Pivot Location and Reduced Pitch Rate on Pitching Rectangular Flat Plates
inferred← citeshttps://doi.org/10.2514/1.j059320openalex-snapshot
Starting Flow by Pitch Acceleration of Flat-Plate Foil
inferred← citeshttps://doi.org/10.2514/3.45178openalex-snapshot
Dynamic overshoot of the static stall angle
inferred← citeshttps://doi.org/10.2514/3.45507openalex-snapshot
Lift-curve characteristics for an airfoil pitching at constant rate
inferred← citeshttps://doi.org/10.2514/3.45621openalex-snapshot
Airfoil dynamic stall at constant pitch rate and high Reynolds number
inferred← citeshttps://doi.org/10.2514/3.46651openalex-snapshot
Moving wall effect in relation to other dynamic stall flow mechanisms
inferred← citeshttps://doi.org/10.2514/3.47030openalex-snapshot
Experimental measurements of dynamic control surface effectiveness
inferred← citeshttps://doi.org/10.2514/6.1985-1773openalex-snapshot
Dynamic stall overshoot of static airfoil characteristics
inferred← citeshttps://doi.org/10.2514/6.1987-1329openalex-snapshot
Airfoil dynamic stall at constant pitch rate and high Reynolds number
inferred← citeshttps://doi.org/10.2514/6.1988-752openalex-snapshot
Toward an unsteady-flow airplane
inferred← citeshttps://doi.org/10.2514/6.1993-3424openalex-snapshot
The moving wall effect vis-a-vis other dynamic stall flow mechanisms
inferred← citeshttps://doi.org/10.2514/6.1996-3407openalex-snapshot
Identification of an unsteady aerodynamic model at high angles of attack
inferred← citeshttps://doi.org/10.2514/6.2006-6001openalex-snapshot
Pitch-Rate Induced Abrupt Wing Stalling of Straight Wing Aircraft
inferred← citeshttps://doi.org/10.2514/6.2009-3686openalex-snapshot
High-Frequency, High-Amplitude Pitch Problem: Airfoils, Plates, and Wings
inferred← citeshttps://doi.org/10.2514/6.2013-2992openalex-snapshot
Effects of Planform Geometry and Pivot Axis Location on the Aerodynamics of Pitching Low Aspect Ratio Wings
inferred← citeshttps://doi.org/10.2514/6.2016-1066openalex-snapshot
Experimental Investigation of Three-Dimensional Flow Development by Pitching Low-Aspect-Ratio Wing
inferred← citeshttps://doi.org/10.6125/15-1123-870openalex-snapshot
Low Reynolds Number Aerodynamics of Finite Wing at Low Reduced Pitch Rates
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