Structural Dynamic Characterization of a Modular Morphing Wing Exploiting Finite Elements and Taguchi Methodology Article Swipe
Faisal Mahmood
,
Seyed M. Hashemi
,
Hekmat Alighanbari
·
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace10040376
YOU?
·
· 2023
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace10040376
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.
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Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.3390/aerospace10040376
- https://www.mdpi.com/2226-4310/10/4/376/pdf?version=1681695669
- OA Status
- gold
- Cited By
- 4
- References
- 24
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4366090424
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Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W4366090424Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.3390/aerospace10040376Digital Object Identifier
- Title
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Structural Dynamic Characterization of a Modular Morphing Wing Exploiting Finite Elements and Taguchi MethodologyWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2023Year of publication
- Publication date
-
2023-04-17Full publication date if available
- Authors
-
Faisal Mahmood, Seyed M. Hashemi, Hekmat AlighanbariList of authors in order
- Landing page
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https://doi.org/10.3390/aerospace10040376Publisher landing page
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https://www.mdpi.com/2226-4310/10/4/376/pdf?version=1681695669Direct link to full text PDF
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goldOpen access status per OpenAlex
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https://www.mdpi.com/2226-4310/10/4/376/pdf?version=1681695669Direct OA link when available
- Concepts
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Morphing, Wing, Modular design, Aeroelasticity, Finite element method, Aerodynamics, Structural engineering, Computer science, Engineering, Aerospace engineering, Artificial intelligence, Operating systemTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
4Total citation count in OpenAlex
- Citations by year (recent)
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2025: 1, 2024: 2, 2023: 1Per-year citation counts (last 5 years)
- References (count)
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24Number of works referenced by this work
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10Other works algorithmically related by OpenAlex
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| abstract_inverted_index.on | 150 |
| abstract_inverted_index.to | 4, 43, 77, 165, 169 |
| abstract_inverted_index.The | 188 |
| abstract_inverted_index.and | 27, 52, 64, 168, 194, 202 |
| abstract_inverted_index.are | 142, 186 |
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| abstract_inverted_index.due | 3, 76 |
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| abstract_inverted_index.its | 44, 78, 112 |
| abstract_inverted_index.the | 5, 9, 59, 91, 97, 120, 123, 151, 170 |
| abstract_inverted_index.to, | 56 |
| abstract_inverted_index.This | 144 |
| abstract_inverted_index.With | 17, 90 |
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| abstract_inverted_index.each | 166 |
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| abstract_inverted_index.eyebolt | 174 |
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| abstract_inverted_index.various | 94 |
| abstract_inverted_index.aviation | 10 |
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| abstract_inverted_index.elements | 163 |
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| abstract_inverted_index.in-house | 133 |
| abstract_inverted_index.industry | 11 |
| abstract_inverted_index.inherent | 79 |
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| abstract_inverted_index.parallel | 155 |
| abstract_inverted_index.research | 136 |
| abstract_inverted_index.spanwise | 203 |
| abstract_inverted_index.adaptable | 35 |
| abstract_inverted_index.condition | 61 |
| abstract_inverted_index.connected | 164 |
| abstract_inverted_index.developed | 132, 148 |
| abstract_inverted_index.different | 30 |
| abstract_inverted_index.embraces, | 51 |
| abstract_inverted_index.increased | 84 |
| abstract_inverted_index.potential | 19 |
| abstract_inverted_index.presented | 206 |
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| abstract_inverted_index.theories, | 179 |
| abstract_inverted_index.vibration | 98, 190 |
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| abstract_inverted_index.experiment | 211 |
| abstract_inverted_index.exploited. | 187 |
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| abstract_inverted_index.prospects, | 68 |
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| abstract_inverted_index.tremendous | 14 |
| abstract_inverted_index.un-morphed | 192 |
| abstract_inverted_index.undergoing | 197 |
| abstract_inverted_index.variations | 62 |
| abstract_inverted_index.Detrimental | 0 |
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| abstract_inverted_index.aerodynamic | 25 |
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| abstract_inverted_index.maneuverability | 28 |
| abstract_inverted_index.re-configurable | 128 |
| abstract_inverted_index.characteristics. | 118 |
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| cited_by_percentile_year.min | 89 |
| corresponding_author_ids | https://openalex.org/A5058247662 |
| countries_distinct_count | 1 |
| institutions_distinct_count | 3 |
| corresponding_institution_ids | https://openalex.org/I530967 |
| citation_normalized_percentile.value | 0.87257616 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |