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.
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Wang, C., Mao, Y., Liu, Q., Fan, S., Shen, X., Zhang, J., & Xia, Y. (2023). Predicting and Reinforcing the Critical Buckling Loads of Flexible Corrugated Panels. Machines, 11(3), 339
All Research
Journal Articles
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Wang, C., Mao, Y., Liu, Q., Fan, S., Shen, X., Zhang, J., & Xia, Y. (2023). Predicting and Reinforcing the Critical Buckling Loads of Flexible Corrugated Panels. Machines, 11(3), 339
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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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Rotor-Wind Interactions under gust and turbulence. (current)
PhDOther supervisor: Dr Alper Celik -
Untitled (current)
MScOther supervisor: Dr Alper Celik -
Untitled (current)
MScOther supervisor: Dr Zhaoxin Ren
Taught Modules
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EG-M330 Next Generation Sustainable Aircraft Technologies
This module will introduce students to leading research technologies that will play a part in enabling future `net zero¿ aircraft using Sustainable Aviation Fuels (SAF), hydrogen-based propulsion, electrification or a combination thereof. After introducing students to the motivation and likely timescales of next generation aircraft utilising these new propulsion approaches the module run as a series of research seminars, including class discussion and Q&A, on technology areas that will be necessary to facilitate practical implementation of future `net zero¿ aircraft. By the end of the module students should have a good understanding of the challenges facing the aerospace industry to achieve sustainable aircraft over the next 2 ¿ 3 decades as well as some of the technologies that will enable the transition.
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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