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Ton Duc Thang University (TDTU) was established on September 24, 1997, as a public university under the Vietnam General Confederation of Labor. After 29 years of development, TDTU has grown into one of the leading universities in Vietnam, with a strong commitment to academic excellence, scientific research, innovation, and international cooperation. With modern facilities, advanced educational programs, and a multidisciplinary approach, TDTU provides a dynamic learning and research environment that promotes creativity and supports the comprehensive development of learners.

Currently, TDTU comprises 16 faculties and offers 52 undergraduate study programs, with a community of more than 77,000 alumni. The University also collaborates with more than 200 adjunct professors and researchers and has produced over 14,200 international publications, reflecting its growing contribution to global academic and scientific communities.

With the vision of becoming a world-class university, TDTU continues to strengthen its educational and research capacity, foster innovation, and enhance international collaboration. The establishment and development of the Journal of Advanced Engineering and Computation (JAEC) represent one of TDTU’s efforts to promote scientific research, disseminate advanced knowledge, and contribute to the development of engineering, technological and interdisciplinary research. More

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  • Vol 4, No 2 (2020)
  • Takizawa
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Computational Flow Analysis in Aerospace, Energy and Transportation Technologies with the Variational Multiscale Methods

Kenji Takizawa, Yuri Bazilevs, Tayfun E. Tezduyar, Artem Korobenko

Abstract


With the recent advances in the variational multiscale (VMS) methods, computational ow analysis in aerospace, energy, and transportation technologies has reached a high level of sophistication. It is bringing solutions in challenging problems such as the aerodynamics of parachutes, thermo-fluid analysis of ground vehicles and tires, and fluid-structure interaction (FSI) analysis of wind turbines. The computational challenges include complex geometries, moving boundaries and interfaces, FSI, turbulent flows, rotational flows, and large problem sizes. The Residual-Based VMS (RBVMS), Arbitrary Lagrangian-Eulerian VMS (ALE-VMS) and Space-Time VMS (ST-VMS) methods have been successfully serving as core methods in addressing the computational challenges. The core methods are supplemented with special methods targeting specific classes of problems, such as the Slip Interface (SI) method, MultiDomain Method, and the ST-C data compression method. We provide and overview of the core and special methods. We present, as examples of challenging computations performed with these methods, aerodynamic analysis of a ramair parachute, thermo-fluid analysis of a freight truck and its rear set of tires, and aerodynamic and FSI analysis of two back-to-back wind turbines in atmospheric boundary layer flow.

Creative Commons License

This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium provided the original work is properly cited.




Keywords


Aerospace technologies, Energy technologies, Transportation technologies, Computational flow analysis, FSI, Space– Time VMS method, ALE-VMS method

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DOI: http://dx.doi.org/10.25073/jaec.202042.279

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Copyright (c) 2020 Journal of Advanced Engineering and Computation

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Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 International License.