The Nusselt number and the aerodynamic coefficients for prolate and cylindrical particles at low to moderate Reynolds number

Dhiraj A. Lote, Xin Yang*, Mohammed Khalij, Boris Arcen, Anne Tanière, Xuerui Mao

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

This work aims to improve existing models for the Nusselt number (Nu), drag coefficient (CD), lift coefficient (CL), and pitching torque coefficient (CT) in flow passing prolate and cylindrical particles by incorporating the effects of particle orientation. Three-dimensional cold flow around hot particles was performed to quantify Nu and aerodynamic coefficients at aspect ratios from 2 to 10, Reynolds number from 0.1 to 300, and orientation from 0°to 90°. The simulation results are validated by Nu, CD, CL, and CT of spherical and non-spherical particles in the literature. Based on the CFD data, a complete set of correlations for Nu, CD, CL, and CT is proposed, demonstrating good performance for the particles considered. Overall, Nu increases with Rep while CD decreases; both Nu and CD increase with incidence angle. The relative difference for Nu, CD, CL, and CT between prolate and cylindrical particles reduces as the aspect ratio increases.

Original languageEnglish
Article number121131
JournalPowder Technology
Volume464
DOIs
Publication statusPublished - Oct 2025

Keywords

  • Drag coefficient
  • Lift coefficient
  • Non-spherical particle
  • Nusselt number
  • Pitching torque coefficient

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