University of Tehran - Iran
Professional Profile
SCOPUS
ORCID
Early Academic Pursuits
Shidvash Vakilipour's academic journey began with a strong focus on mechanical engineering, obtaining a B.Sc. from Sharif University of Technology in September 2000. He further specialized in aerodynamic engineering with an M.Sc. from Tarbiat Modares University, completed in January 2003. His pursuit of advanced knowledge led him to earn a Ph.D. in Power and Propulsion from Sharif University of Technology in September 2008. This academic background laid the foundation for his expertise in computational fluid dynamics, thermo-fluid science, and propulsion systems.
Professional Endeavors
Vakilipour's professional career is marked by significant academic and research positions. He is an Associate Professor at the College of Interdisciplinary Science and Technology, University of Tehran, where he also served as Executive Vice President. His experience includes a post-doctoral research fellowship at the University of Manitoba, where he contributed to the Computational Thermo-Fluid Science Lab. His roles have allowed him to mentor graduate students and lead significant research projects in computational fluid dynamics and thermo-fluid sciences.
Contributions and Research Focus
Vakilipour has made notable contributions to computational thermo-fluid science, focusing on numerical simulations of multi-phase flows, aero-thermal flow calculations in turbomachinery, turbulence flow modeling, and molecular dynamics simulations. His research extends to power and propulsion systems, Engineering including engine condition trend monitoring and performance enhancement of gas turbine-based power plants. He is also involved in renewable energy technologies, such as wind turbine blade design and combustion modeling for sustainable energy applications. His work is supported by extensive use of scientific computing software like OpenFOAM, Fluent, and CFX.
Accolades and Recognition
Vakilipour's achievements include membership in the Canadian Society for Mechanical Engineering and a post-doctoral research fellowship at the University of Manitoba. He founded The Center for High Performance Computing at the University of Tehran, Engineering demonstrating his leadership in advancing computational research infrastructure. His role as a visiting researcher at the University of Manitoba underscores his international recognition and collaboration in the field of mechanical engineering.
Impact and Influence
Vakilipour's research has had a significant impact on the fields of thermo-fluid dynamics and propulsion systems. His work on numerical simulations and turbulence modeling has contributed to advancements in the efficiency and performance of engineering systems. His academic contributions are further amplified by his role in mentoring Ph.D. and M.Sc. students, guiding their research in complex fluid dynamics and energy systems. His publications and collaborations reflect his influence on both the academic community Engineering and industry applications.
Legacy and Future Contributions
Shidvash Vakilipour's legacy is characterized by his dedication to advancing computational and experimental methods in mechanical engineering. His ongoing research projects, such as the development of interface tracking methods for two-phase flows and the aerodynamic assessment of wind turbine airfoils, promise to push the boundaries of current engineering knowledge. His future contributions are anticipated to further enhance the understanding and application of thermo-fluid dynamics in renewable energy and propulsion systems.
NOTABLE PUBLICATIONS
A fully coupled ALE interface tracking method for a pressure-based finite volume solver 2021(5)
Numerical study of longitudinal vein effects on the aerodynamic characteristics of a corrugated bio-airfoil 2021(2)
Inverse Designing Airfoil Aerodynamics in Compressible Flow by Target Pressure Distribution 2021(1)
A numerical investigation of CO2 dilution on the thermochemical characteristics of a swirl stabilized diffusion flame 2020(2)
Numerical assessment of a deformable trailing-edge flap on aerodynamic load control of a pitching S809 airfoil using OpenFOAM 2016(7)