Aeroelastic Simulation of High-Aspect Ratio Wings with Intermittent Leading-Edge Separation
Author:
Affiliation:
1. University of Warwick, Coventry, England CV4 7AL, United Kingdom
2. Imperial College, London, England SW7 2AZ, United Kingdom
3. Tohoku University, Sendai 980-8579, Japan
Funder
Leverhulme Trust
UK Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060909
Reference22 articles.
1. State-Space Realizations and Internal Balancing in Potential-Flow Aerodynamics with Arbitrary Kinematics
2. Three-dimensional viscous-inviscid coupling method for wind turbine computations
3. Aerodynamic load control in horizontal axis wind turbines with combined aeroelastic tailoring and trailing-edge flaps
4. Nonlinear-Aerodynamics/Nonlinear-Structure Interaction Methodology for a High-Altitude Long-Endurance Wing
5. Stall Recovery of a Morphing Wing via Extended Nonlinear Lifting-Line Theory
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