Effect of engine location on flutter speed and frequency of a tapered viscoelastic wing Article Swipe
Youssef S. Matter
,
Tariq Darabseh
,
Abdel‐Hamid I. Mourad
·
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1088/1757-899x/370/1/012014
YOU?
·
· 2018
· Open Access
·
· DOI: https://doi.org/10.1088/1757-899x/370/1/012014
The flutter of a tapered viscoelastic wing carrying an engine and subjected to a follower thrust force is investigated. The wing is considered as a cantilever tapered Euler-Bernoulli beam, made of a linear viscoelastic material where Kelvin-Voigt model is assumed to represent the viscoelastic behaviour of the material. In addition, quasi-steady and unsteady aerodynamic forces models are introduced along with the follower thrust force. The mass and inertia of the engine are modelled in order to achieve more realistic behaviour of the engine upon flutter characteristics of the system. Moreover, the governing equations of motion are derived through the Extended Hamilton's Principle. The generalized function theory is used to more accurately consider the contribution of the mass and its follower force in the governing equations. The resulting partial differential equations are solved by Galerkin method along with the classical flutter investigation approach. Parametric studies highlighting the sensitivity of the chord-wise engine location, the span-wise engine location, and the vertical engine location on the flutter speed and flutter frequency are reported. It is found that the location of the engine in the three directions play an important role in the dynamic stability of the wing.
Related Topics
Concepts
Flutter
Aeroelasticity
Aerodynamic force
Thrust
Viscoelasticity
Mechanics
Equations of motion
Aerodynamics
Inertia
Timoshenko beam theory
Structural engineering
Control theory (sociology)
Classical mechanics
Mathematics
Physics
Engineering
Computer science
Beam (structure)
Aerospace engineering
Thermodynamics
Control (management)
Artificial intelligence
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1088/1757-899x/370/1/012014
- OA Status
- diamond
- Cited By
- 3
- References
- 20
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W2775948011
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W2775948011Canonical identifier for this work in OpenAlex
- DOI
-
https://doi.org/10.1088/1757-899x/370/1/012014Digital Object Identifier
- Title
-
Effect of engine location on flutter speed and frequency of a tapered viscoelastic wingWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2018Year of publication
- Publication date
-
2018-05-01Full publication date if available
- Authors
-
Youssef S. Matter, Tariq Darabseh, Abdel‐Hamid I. MouradList of authors in order
- Landing page
-
https://doi.org/10.1088/1757-899x/370/1/012014Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
-
diamondOpen access status per OpenAlex
- OA URL
-
https://doi.org/10.1088/1757-899x/370/1/012014Direct OA link when available
- Concepts
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Flutter, Aeroelasticity, Aerodynamic force, Thrust, Viscoelasticity, Mechanics, Equations of motion, Aerodynamics, Inertia, Timoshenko beam theory, Structural engineering, Control theory (sociology), Classical mechanics, Mathematics, Physics, Engineering, Computer science, Beam (structure), Aerospace engineering, Thermodynamics, Control (management), Artificial intelligenceTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
3Total citation count in OpenAlex
- Citations by year (recent)
-
2022: 1, 2021: 1, 2018: 1Per-year citation counts (last 5 years)
- References (count)
-
20Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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| primary_location.source.host_organization_lineage_names | IOP Publishing, Institute of Physics |
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| publication_date | 2018-05-01 |
| publication_year | 2018 |
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