Active aeroelastic tailoring of high aspect ratio composite wings

Author:

Cesnik Carlos1,Ortega-Morales Miguel1,Patil Mayuresh1

Affiliation:

1. MIT, Cambridge, MA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 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. Conventional and Unconventional Control Effectors for Load Alleviation in High-Aspect-Ratio-Wing Aircraft;AIAA SCITECH 2022 Forum;2022-01-03

2. Influence of Aileron Placement on Roll Response of High-Aspect-Ratio-Wing Aircraft;AIAA AVIATION 2020 FORUM;2020-06-08

3. MDO/MSO of Slender Thin Walled Box Beam Model;18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2017-06-02

4. Design of Composite Structures to Improve the Aeroelastic Performance;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

5. Design-Oriented Structural Model Order Reduction for Strain-Actuated Flight Vehicle Structures;Journal of Aircraft;2006-01

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