Aeroservoelastic tailoring for gust response of a typical section aeroelastic model-Reference-Cited by-同舟云学术

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Aeroservoelastic tailoring for gust response of a typical section aeroelastic model

Published:1995-04-10 Issue: Volume: Page:
ISSN:
Container-title:36th Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

Layton Jeffrey

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1192

Reference22 articles.

1. Aeroelastic Tailoring of Forward Swept Composite Wings

2. Exploratory design studies of actively controlled wings using integrated multidisciplinary synthesis

Cited by 6 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. Gradient-Based Aeroservoelastic Optimization with Static Output Feedback;Journal of Guidance, Control, and Dynamics;2019-10

2. Gradient-Based Aeroservoelastic Optimization with Static Output Feedback;AIAA Scitech 2019 Forum;2019-01-06

3. Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces;Journal of Aircraft;2016-07

4. Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces;33rd AIAA Applied Aerodynamics Conference;2015-06-19

5. Theoretical and Experimental Study of Gust Response Alleviation Using Neuro-fuzzy Control Law for a Flexible Wing Model;Chinese Journal of Aeronautics;2010-06

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