Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap Static Aeroelastic Action-Reference-Cited by-同舟云学术

Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap Static Aeroelastic Action

Published:2017-03 Issue:3 Volume:55 Page:1031-1043
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Yan¹,Bai Junqiang¹,Livne Eli²

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. University of Washington, Seattle, Washington 98195

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J055054

Reference34 articles.

1. Aeroelastic Modeling of Elastically Shaped Aircraft Concept via Wing Shaping Control for Drag Reduction

2. NguyenN.UrnesJ. “A Mission Adaptive Variable Camber Flap Control System to Optimize High Lift and Cruise Lift to Drag Ratios of Future N+3 Transport Aircraft,” AIAA Paper 2013-214, 2013. doi:10.2514/6.2013-214

3. Initial Assessment of a Variable-Camber Continuous Trailing-Edge Flap System for Drag-Reduction of Non-Flexible Aircraft in Steady-State Cruise Condition

4. Aeroelastic Modeling and Drag Optimization of Flexible Wing Aircraft with Variable Camber Continuous Trailing Edge Flap

5. Drag Optimization Study of Variable Camber Continuous Trailing Edge Flap (VCCTEF) Using OVERFLOW

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