Numerical investigation of steady and unsteady state hopper flows

H. P. Zhu, A. B. Yu, Y. H. Wu

Research output: Contribution to journalArticleResearchpeer-review

38 Citations (Scopus)

Abstract

This paper presents a numerical study of the steady and unsteady state granular flows in a cylindrical hopper with flat bottom by means of the discrete element method (DEM). For both flows, the simulations were conducted under comparable conditions so that the similarity and difference between them can be examined. The distributions of the physical properties including velocity, force structure, stress and couple stress for the two hopper flows are investigated. The results suggest that the trends of these distributions for the two hopper flows are similar. In particular, for both cases, the distributions of the normal stresses are related to the normal force structures. Thus, corresponding to the large interaction forces between particles near the bottom corner and in the transitional zone, all the normal stresses are large near the bottom corner, and the radial and circumferential normal stresses are relatively large in the transitional zone. However, there are differences in the magnitudes of some physical properties for the unsteady and steady state flows. Compared with the steady state flow, the unsteady state flow has a narrower velocity distribution, and more particles experience large contact forces. Its radial and circumferential normal stresses in the plug flow and transitional zones are larger. With the decrease of the number of particles or with discharging time, the plug flow and transitional zones reduce, and the differences in the considered properties except wall shear stress and couple stress between the two flows decrease.

Original languageEnglish
Pages (from-to)125-134
Number of pages10
JournalPowder Technology
Volume170
Issue number3
DOIs
Publication statusPublished - 14 Dec 2006
Externally publishedYes

Keywords

  • Continuum approach
  • Discrete element method
  • Granular matter
  • Hopper flow

Cite this