Recent Advances in Computational Fluid Dynamics

A special issue of Fluids (ISSN 2311-5521). This special issue belongs to the section "Mathematical and Computational Fluid Mechanics".

Deadline for manuscript submissions: closed (31 October 2022) | Viewed by 5581

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Guest Editor
Department of Mathematics and Statistical Sciences, Jackson State University, Jackson, MS 39217, USA
Interests: computational fluid dynamics; flow control; turbulence; shock boundary layer interaction
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Special Issue Information

Dear Colleagues,

Since its development, computational fluid dynamics (CFD) has become an important research tool in various disciplines and industries, including aerospace, automotive, power generation, chemical manufacturing, polymer processing, petroleum exploration, medical research, meteorology, and celestial bodies physics. Vortices are the building blocks of complex flows. Although there are still many issues to be explored, CFD has special advantages for use in complex flow systems, especially ones containing complex vortex structures.

This Special Issue of Fluids is dedicated to the latest developments in CFD, especially those involving the scientific research of vortex structures and their applications in industrial engineering. All numerical methods, including the finite difference method, the finite volume method, the finite element method, and the Lattice Boltzmann method, are welcome.

Dr. Yonghua Yan
Guest Editor

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Keywords

  • computational fluid dynamics
  • aerospace
  • automotive
  • power generation
  • chemical manufacturing
  • polymer processing
  • complex flows

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Published Papers (2 papers)

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Research

16 pages, 9180 KiB  
Article
Study on the Sensitivity of the Streamwise Location of MVG on SWBLI in MVG-Based Supersonic Flow Control
by Yonghua Yan, Demetric L. Baines, Yong Yang, Caixia Chen and Tor A. Kwembe
Fluids 2022, 7(9), 285; https://doi.org/10.3390/fluids7090285 - 23 Aug 2022
Viewed by 1632
Abstract
Micro vortex generator (MVG) is a currently facile, robust, and feasible device for supersonic and hypersonic flow control. The purpose of this study is to investigate the impact on SWBLI from the streamwise location of MVG. Large eddy simulation (LES) was conducted on [...] Read more.
Micro vortex generator (MVG) is a currently facile, robust, and feasible device for supersonic and hypersonic flow control. The purpose of this study is to investigate the impact on SWBLI from the streamwise location of MVG. Large eddy simulation (LES) was conducted on MVG controlled supersonic ramp flow to reveal the sensitivity of MVG streamwise position on shock-wave boundary-layer interaction (SWBLI) control. Numerical cases with minor different distances between MVG and ramp corner are carried out. The results are analyzed in time-averaged and instantaneous view, respectively. The results show that streamwise position has a significant effect on SWBLI in some aspects. With minor changes on the streamwise position, the ring-like vortices generated by MVG were very similar, with only small changes in height and intensity. However, the small changes made on the ring-like vortices produced relatively significant changes to the separation region in front of the ramp. In terms of the time-averaged solution, the farther the MVG is from the ramp, the higher the ring-like vortices are lifted, and the shock wave is also disturbed/reduced more strongly. Further, the flow separation zone on the wall also appears smaller. The results of this study play a guiding role for further optimal configuration of MVG in flow control. Full article
(This article belongs to the Special Issue Recent Advances in Computational Fluid Dynamics)
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17 pages, 4812 KiB  
Article
Numerical Analysis for Augmentation of Thermal Performance of Single-Phase Flow in Microchannel Heat Sink of Different Sizes with or without Micro-Inserts
by Shailesh Ranjan Kumar and Satyendra Singh
Fluids 2022, 7(5), 149; https://doi.org/10.3390/fluids7050149 - 24 Apr 2022
Cited by 6 | Viewed by 2468
Abstract
With the development of miniaturized and enormous heat density generating novel technologies, the microchannel heat sink is rapidly establishing itself in modern cooling fields. Enhancement of heat transfer performance of microchannels is done by incorporating improved design structure, changing working fluids and flow [...] Read more.
With the development of miniaturized and enormous heat density generating novel technologies, the microchannel heat sink is rapidly establishing itself in modern cooling fields. Enhancement of heat transfer performance of microchannels is done by incorporating improved design structure, changing working fluids and flow conditions, using different materials for fabrication, etc. Coupling of two parameters influencing heat transfer performance of microchannels is in a nascent age, and complex coupling of heat transfer influencing parameters of microchannel sinks has not been clearly understood yet. This study provides the thermal-fluid flow features–fluid flow characteristics and heat transfer characteristics- of single-phase flow in microchannel of different sizes with or without microinserts by the use of computational fluid dynamics. The numerical simulation is performed by employing distilled water with thermophysical properties that depends on temperature for the Reynolds number range of 56–2242. The effect of microinserts on characteristics of fluid flow and heat transfer is analyzed. The results of numerical analysis show that heat transfer performance in microchannel with microinserts is enhanced effectively, however resistance in fluid flow is increased simultaneously. The 0.5 mm microchannel with microinserts shows the best performance of heat transfer characteristics with enhancement of 1–9% in the Reynolds number range of 56–2242 with simultaneous maximum increase in pressure drop by 14.5%. It’s overall performance, evaluated by thermal performance factor, is found to be best among all cases of three different channel sizes with and without microinserts. The maximum enhancement of heat transfer is found to be in case of 0.5 mm channel size with microinserts by a factor of 1.09. The maximum pressure drop is increased is found to be by factor of 2.28 in case of 2 mm channel size with microinserts. Full article
(This article belongs to the Special Issue Recent Advances in Computational Fluid Dynamics)
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