Conceptual Design and Experimental Demonstration of a Distributedly Actuated Morphing Wing-Reference-Cited by-同舟云学术

Conceptual Design and Experimental Demonstration of a Distributedly Actuated Morphing Wing

Published:2015-03 Issue:2 Volume:52 Page:452-461
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Zhang Ping¹,Zhou Li¹,Cheng Wenjie¹,Qiu Tao²

Affiliation:

1. College of Aerospace Engineering, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

2. Department of Synthetic Strength, Aviation Industry Corporation of China, 110035 Shenyang, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032739

Reference22 articles.

1. A Review of Morphing Aircraft

2. Morphing Aircraft Technology Survey

3. Shape morphing of aircraft wing: Status and challenges

4. WeisshaarT. A. “Morphing Aircraft Technology-New Shapes for Aircraft Design,” Proceedings of the Multifunctional Structures/Integration of Sensors and Antennas, RTO-MP-AVT-141, RTO, Neuilly-sur-Seine, France, 2006, pp. O1-1–O1-20.

5. HallJ. M. “Executive Summary AFTI/F-111 Mission Adaptive Wing,” Wright Research Development Center, Rept. WRDC TR-89-2083, Wright–Patterson AFB, OH, 1989.

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