Structural Dynamic Characterization of a Modular Morphing Wing Exploiting Finite Elements and Taguchi Methodology

Author:

Mahmood Faisal1,Hashemi Seyed M.1ORCID,Alighanbari Hekmat1

Affiliation:

1. Department of Aerospace Engineering, Toronto Metropolitan University, Toronto, ON M5B 2K3, Canada

Abstract

Detrimental environmental impacts due to the increasing demands of the aviation industry have gained tremendous global attention. With a potential fuel saving, along with high aerodynamic performance and maneuverability during different phases of a flight, adaptable wing design has become a viable alternative to its fixed-shape counterpart. A morphing wing design embraces, and can respond accordingly to, most of the flight condition variations effectively and efficiently. Despite these prospects, morphing wing design comes with some challenges due to its inherent complexity caused by an increased number of degrees of freedom. With the availability of various morphing parameters, the vibration signature of a morphing wing design plays a vital role in terms of its structural as well as aeroelastic characteristics. In the present paper, the dynamic characteristics of a re-configurable modular morphing wing developed in-house by a research team at Toronto Metropolitan University are investigated. This modular morphing wing, developed based on the idea of a parallel robot, consists of a number of structural elements connected to each other and to the wing ribs through eyebolt joints. Timoshenko bending beam theories, in conjunction with finite element methodology, are exploited. The free vibration of un-morphed (original) and morphed configurations undergoing multiple levels of sweep and spanwise morphing is presented through a design of experiment methodology.

Funder

Discovery Grant from the Natural Sciences and Engineering Research Council of Canada

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference34 articles.

1. Arena, M., Amoroso, F., Pecora, R., and Ameduri, S. (2019). Electro-Actuation System Strategy for a Morphing Flap. Aerospace, 6.

2. ICAO (2016). Resolution A39-3: Consolidated Statement of Continuing ICAO Policies and Practices Related to Environmental Protection—Global Market-Based Measure (MBM) Scheme, International Civil Aviation Organization. Technical Report.

3. ICAO (2010). ICAO: 37th Assembly Working Papers, A37-WP/402, Report of the Executive Committee on Agenda Item 17, Section on Climate Change, Montreal, International Civil Aviation Organization. Technical Report.

4. IATA (2013). IATA Technology Roadmap, International Air Transport Association. [4th ed.].

5. Multipoint Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft;Li;J. Aircraft,2022

Cited by 1 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

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3