Variable-Fidelity Kinematic Optimization of a Two-Dimensional Hovering Wing-Reference-Cited by-同舟云学术

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Variable-Fidelity Kinematic Optimization of a Two-Dimensional Hovering Wing

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Moore John¹,Stanford Bret¹,McClung Aaron¹,Beran Philip¹

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1245

Reference25 articles.

1. Computational aerodynamics of low Reynolds number plunging, pitching and flexible wings for MAV applications

2. Energy-minimizing kinematics in hovering insect flight

3. Modelization and Kinematics Optimization for a Flapping-Wing Microair Vehicle

4. Optimal actuation of nonlinear resonant systems

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multi-infill strategy for kriging models used in variable fidelity optimization;Chinese Journal of Aeronautics;2018-03

2. Design of Airfoils in Unsteady Viscous Flows Using Hierarchical Kriging Model;55th AIAA Aerospace Sciences Meeting;2017-01-05

3. Global optimization of actively morphing flapping wings;Journal of Fluids and Structures;2012-08

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