About
Dr Yuying Xia is a Senior Lecturer in Aerospace Engineering.
Dr Yuying Xia
Associate Professor
Aerospace Engineering
Office - 327
Third Floor
Engineering North
Bay Campus
Third Floor
Engineering North
Bay Campus
Available For Postgraduate Supervision
Publications
Research Highlights
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Zhang, Q., Yu, X., Scarpa, F., Barton, D., Xia, Y., Shaw, A., Zhu, Y., & Lang, Z. (2023). Hysteretic behaviour of uniaxially thermoformed auxetic foams under 3-point bending low-frequency vibration. Nonlinear Dynamics, 111(2), 1019-1045.
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Pan, C., Jiang, J., Zhang, R., & Xia, Y. (2021). Closed‐form design formulae for seismically isolated structure with a damping enhanced inerter system. Structural Control and Health Monitoring, 28(12)
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Zhao, Z., Chen, Q., Zhang, R., Jiang, Y., & Xia, Y. (2020). Interaction of Two Adjacent Structures Coupled by Inerter-based System considering Soil Conditions. Journal of Earthquake Engineering, 1-21.
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Wang, C., Xia, Y., Friswell, M., & Flores, E. (2019). Predicting Global Strain Limits for Corrugated Panels. Composite Structures, 111472
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Chen, Q., Zhao, Z., Xia, Y., Pan, C., Luo, H., & Zhang, R. (2019). Comfort based floor design employing tuned inerter mass system. Journal of Sound and Vibration, 458, 143-157.
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Wang, C., Haddad Khodaparast, H., Friswell, M., Shaw, A., Xia, Y., & Walters, P. (2018). Development of a morphing wingtip based on compliant structures. Journal of Intelligent Material Systems and Structures, 29(16), 3293-3304.
All Research
Journal Articles
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Zhang, Q., Yu, X., Scarpa, F., Barton, D., Xia, Y., Shaw, A., Zhu, Y., & Lang, Z. (2023). Hysteretic behaviour of uniaxially thermoformed auxetic foams under 3-point bending low-frequency vibration. Nonlinear Dynamics, 111(2), 1019-1045.
-
Pan, C., Jiang, J., Zhang, R., & Xia, Y. (2021). Closed‐form design formulae for seismically isolated structure with a damping enhanced inerter system. Structural Control and Health Monitoring, 28(12)
-
Zhao, Z., Chen, Q., Zhang, R., Jiang, Y., & Xia, Y. (2020). Interaction of Two Adjacent Structures Coupled by Inerter-based System considering Soil Conditions. Journal of Earthquake Engineering, 1-21.
-
Wang, C., Xia, Y., Friswell, M., & Flores, E. (2019). Predicting Global Strain Limits for Corrugated Panels. Composite Structures, 111472
-
Chen, Q., Zhao, Z., Xia, Y., Pan, C., Luo, H., & Zhang, R. (2019). Comfort based floor design employing tuned inerter mass system. Journal of Sound and Vibration, 458, 143-157.
-
Wang, C., Haddad Khodaparast, H., Friswell, M., Shaw, A., Xia, Y., & Walters, P. (2018). Development of a morphing wingtip based on compliant structures. Journal of Intelligent Material Systems and Structures, 29(16), 3293-3304.
Supervision
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Effects of rotor-wing interaction in gust and turbulent flow. (current)
PhDOther supervisor: Dr Alper Celik
Taught Modules
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EG-263 Engineering Design 2
Within this module students will be expected to work in groups to achieving a solution to a specific design problem involving a multi-disciplinary approach. Projects will involve conceptual, preliminary and detailed design and analysis of wing, horizontal and vertical stabilizer for a light-single engine aircraft, based on their review (or reverse engineering) of an existing aircraft they chose. Projects will run as part of industry-based design projects. Students will be required to produce highly technical design concepts. Each student will be required to take responsibility for particular and defined aspects of the design during the term which will form an important part of the assessment process. The work is presented with an overview of the team project, but with particular detail paid to the individual student contributions.
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EG-D02 MSc Dissertation - Aerospace Engineering
The module aims to develop fundamental research skills. It comprises the development of supervised research work leading to a dissertation in the field of the Master's degree programme. The specific research topic will be chosen by the student following consultation with academic staff.
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EG-M339 Spacecraft Structure Design
This module aims to introduces the fundamental concepts of spacecraft structure design. The structure design process, from spacecraft configuration, initial design, detailed analysis, production of structure and testing, is introduced, which provides insight into the structure design and analysis aspects of spacecraft. The content includes: · Spacecraft structure design process · Spacecraft Design Loads · Tests and Verifications · Deployable Structures and Mechanisms