Aerodynamic Analysis of a harmonically Morphing Flap Using a Hybrid Turbulence Model and Dynamic Meshing
Author:
Affiliation:
1. University of the West of England
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3813
Reference29 articles.
1. Morphing Airfoil Shape Change Optimization With Minimum Actuator Energy As An Objective
2. A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft
3. Optimization and design of an aircraft’s morphing wing-tip demonstrator for drag reduction at low speed, Part I – Aerodynamic optimization using genetic, bee colony and gradient descent algorithms
4. Performance Comparison between Optimised Camber and Span for a Morphing Wing
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