Multidisciplinary Multifidelity Optimisation of a Flexible Wing Aerofoil for Small UAV-Reference-Cited by-同舟云学术

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Multidisciplinary Multifidelity Optimisation of a Flexible Wing Aerofoil for Small UAV

Published:2012-09-11 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Berci Marco¹,Toropov Vassili¹,Hewson Robert¹,Gaskell Philip¹

Affiliation:

1. University of Leeds

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5400

Reference58 articles.

1. Adaptive Aeroelastic Structures

2. 2Sun,J.Q.,StochasticDynamicsandControl,Elsevier,2006.

3. 3Hathaway, E., Active and Passive Techniques for Tiltrotor Aeroelastic Stability Augmentation, PhD Thesis,PennsylvaniaState University,2005.

4. 4Bungartz,H.J.,Schafer,M.,Fluid-StructureInteraction:Modelling,Simulation,Optimization,Springer,2006.

5. Low-Speed Aeroelastic Modeling of Very Flexible Slender Wings with Deformable Airfoils

Cited by 2 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. Multidisciplinary multifidelity optimisation of a flexible wing aerofoil with reference to a small UAV;Structural and Multidisciplinary Optimization;2014-05-21

2. Multidisciplinary Multifidelity Optimisation of a Flexible Wing Aerofoil for Small UAV;12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2012-09-11

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