Gust mitigation with an oscillating airfoil at low Reynolds number
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Maryland, Baltimore County, Baltimore, Maryland 21250, USA
2. DEVCOM—Army Research Lab, Aberdeen Proving Ground, Maryland 21005, USA
Funder
Army Research Laboratory
National Science Foundation
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
https://aip.scitation.org/doi/am-pdf/10.1063/5.0065234
Reference63 articles.
1. Recent progress in flapping wing aerodynamics and aeroelasticity
2. Flapping Wing Aerodynamics: Progress and Challenges
3. MTV measurements of the vortical field in the wake of an airfoil oscillating at high reduced frequency
4. High-fidelity simulations of moving and flexible airfoils at low Reynolds numbers
5. Reynolds number, thickness and camber effects on flapping airfoil propulsion
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