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Airfoil dynamic stall at constant pitch rate and high Reynolds number

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What this work says

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

inferredcites →https://doi.org/10.1007/978-3-642-85829-1openalex-snapshot
Boundary-Layer Theory
inferredcites →https://doi.org/10.2514/3.45050openalex-snapshot
Experimental investigation of dynamic stall for a pitching airfoil
inferredcites →https://doi.org/10.2514/3.45426openalex-snapshot
Aerodynamic testing at low Reynolds numbers
inferredcites →https://doi.org/10.2514/3.45507openalex-snapshot
Lift-curve characteristics for an airfoil pitching at constant rate
inferredcites →https://doi.org/10.2514/3.61332openalex-snapshot
Dynamic Stall Experiments on Oscillating Airfoils
inferredcites →https://doi.org/10.2514/3.9146openalex-snapshot
Airfoil dynamic stall performance with large-amplitude motions
inferredcites →https://doi.org/10.2514/3.9673openalex-snapshot
Force coefficients for a NACA-0015 airfoil undergoing constant pitchrate motions
inferredcites →https://doi.org/10.2514/6.1986-117openalex-snapshot
Lift-curve characteristics for an airfoil pitching at constant rate
inferredcites →https://doi.org/10.4050/jahs.13.49openalex-snapshot
Dynamic Stall Considerations in Helicopter Rotors
inferredcites →https://doi.org/10.4050/jahs.14.26openalex-snapshot
Dynamic Stall of Airfoil Sections for High‐Speed Rotors

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

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Dynamic-Stall-Driven Vertical Axis Wind Turbine: An Experimental Study
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Correlation of Pressure and Hot Film Data on an Oscillating 2D NACA63A006 Single Airfoil at High Incidence
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Computational and experimental studies of compressible dynamic stall
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Numerical investigation of the effect of airfoil thickness on onset of dynamic stall
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Vortex formation on a pitching aerofoil at high surging amplitudes
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Experimental Study on Multiobjective Flow Control of Dynamic Stalls Using a Vortex Generator
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Dynamic Stall Mitigation Using a Deflectable Leading Edge: The IK30 Mechanism
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Dynamic testing in wind tunnels using the wind-driven manipulator
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A New Stall-Onset Criterion for Low Speed Dynamic-Stall
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Active Flow Control of Dynamic Stall by Means of Continuous Jet Flow at Reynolds Number of 1 × 106
inferred← citeshttps://doi.org/10.1146/annurev-fluid-010814-013632openalex-snapshot
Dynamic Stall in Pitching Airfoils: Aerodynamic Damping and Compressibility Effects
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MODERN HELICOPTER AERODYNAMICS
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Dynamic- and post-stall characteristics of pitching airfoils at extreme conditions
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2D Dynamic Stall Simulations with Time-Varying Freestream Representative of Helicopter Flight
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Separation Control Using Plasma Actuators: Dynamic Stall Vortex Control on Oscillating Airfoil
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Investigation of Three-Dimensional Dynamic Stall Using Computational Fluid Dynamics
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Investigation of Spanwise End Effects on Dynamic Stall of a Pitching Wing Section
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Study on a Pitching Natural-Laminar-Flow-0414 Airfoil at Low Reynolds Number
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Improved Understanding of Aerodynamic Damping Through the Hilbert Transform
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Aerodynamics of a Pitching and Heaving Airfoil in Ground Effect
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Effects of Pivot Location and Reduced Pitch Rate on Pitching Rectangular Flat Plates
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Rotating Blade Stall Maps Measured by Differential Infrared Thermography
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Analysis of Tip Vortex Near-Wake Evolution for Stationary and Oscillating Wings
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Analysis of Dynamic Stall on a Pitching Airfoil Using High-Fidelity Large-Eddy Simulations
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Unsteady Flow Physics of Airfoil Dynamic Stall
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Effects of Leading-Edge Geometry on the Onset of Dynamic Stall
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Dynamic Stall of a Finite-Aspect-Ratio Wing
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Effects of Compressibility on Dynamic-Stall Onset Using Large-Eddy Simulation
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Dynamic Stall over a Pitching Natural-Laminar-Flow Airfoil
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Pitch–Plunge Equivalence in Dynamic Stall of Ramp Motion Airfoils
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Dynamic Leading-Edge Flap Scheduling
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Freestream Disturbance Effects on an Airfoil Pitching at Constant Rate
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Boundary-Layer Transition, Separation, and Reattachment on an Oscillating Airfoil
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Initial acceleration effects on flow evolution around airfoils pitching to high angles of attack
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Interferometric investigations of compressible dynamic stall over a transiently pitching airfoil
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Unsteady aerodynamic gust response including steady flow separation
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Interactive boundary-layer method for unsteady airfoil flows - Quasisteady model
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Aerodynamic testing at low Reynolds numbers
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Quantitative study of unsteady compressible flow on an oscillating airfoil
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Study of dynamic stall using real-time interferometry
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Decay of Aircraft Vortices near the Ground
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Aeroelasticity and Unsteady Aerodynamics
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Compressible studies on dynamic stall
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Two dimensional post stall maneuver of a NACA 0015 airfoil at high pitching rates
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A quantitative study of unsteady compressible flow on an oscillatingairfoil
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Dynamic stall experiments on a swept three-dimensional wing in compressible flow
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A study of dynamic stall using real time interferometry
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Incipient torsional stall flutter aerodynamic experiments on a sweptthree-dimensional wing
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Interferometric investigations of compressible dynamic stall over a transiently pitching airfoil
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PSP Measurements on an Oscillating NACA 0012 Airfoil in Compressible Flow
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Dynamic Stall over a Pitching Natural-Laminar-Flow Airfoil
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Pitch-plunge Equivalence in Dynamic Stall of Ramp Motion Airfoils
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Prediction of UH-60A Dynamic Stall Loads in High Altitude Level Flight Using CFD/CSD Coupling
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