Abstract

This work displays a numerical and experimental investigation on the flow and heat transfer in tree-like branching microchannels and studies the effects of dimples on the heat transfer enhancement. The numerical approach is certified by a smooth branching microchannel experiment. The verification result shows that the SSG turbulence model can provide a reasonable prediction. Thus, further research on the convective heat transfer in dimpled branching microchannels is conducted with the SSG turbulence model. The results indicate that the dimples can significantly improve the averaged heat transfer performance of branching microchannels, and the heat transfer increment of the branch segment increases with the increase in the branching level. However, the flow dead zones in some dimples at bifurcations and bends suppress the turbulent flow and heat transfer. Furthermore, the Nu number ratio (Nua/Nus) and thermal enhancement factor (η) both monotonously decrease as the Re number increases, while the friction factor ratio (fa/fs) changes nonlinearly. The entropy generation rates of and in all dimpled cases are lower than those in the smooth case, and the dimpled case with the streamwise spacing to diameter ratio s/D = 3 obtains the lowest value of augmentation entropy generation (Ns) under the high Re number conditions. Nua/Nus, fa/fs, and η decline with the increase in the streamwise spacing to diameter ratio (s/D) from 3 to 9; therefore, the dimpled case with s/D = 3 shows the best overall thermal performance.

Highlights

  • The modern gas turbine is the core of advanced energy power systems

  • The entropy generation rates of Ṡt and Ṡ p in all dimpled cases are lower than those in the smooth case, and the dimpled case with the streamwise spacing to diameter ratio s/D = 3 obtains the lowest value of augmentation entropy generation (Ns ) under the high Re number conditions

  • Nua /Nus, f a /f s, and η decline with the increase in the streamwise spacing to diameter ratio (s/D) from 3 to 9; the dimpled case with s/D = 3 shows the best overall thermal performance

Read more

Summary

Introduction

The modern gas turbine is the core of advanced energy power systems. Its thermal efficiency and power output increase as gas inlet temperature rises. The hot gas temperature is far more beyond the melting point of the blade material. The blades need to be cooled by an efficient and reliable cooling system [1]. The research interests regarding cooling technology mainly include the optimization of cooling structure parameters, the improvement of complex cooling strategies, and the development of new cooling technologies based on innovation cooling theories. The dimple cooling technology and the microchannel cooling technology both show remarkable cooling performance

Methods
Results
Conclusion

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.