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Experimental study on velocity deficits of near-limit detonation waves initiated in narrow channels

  • Yuefei Xiong
  • , Hung Ping Chan
  • , Ming Hsun Wu*
  • , Jiang Qin
  • , Chien Fu Chen
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • National Cheng Kung University
  • National Taiwan University

Research output: Contribution to conferencePaperpeer-review

Abstract

The effect of channel size and equivalence ratio of ethylene/oxygen mixtures on detonation velocity deficits were experimentally investigated in miniature square channels in this paper. The premix mixtures were spark ignited under ambient pressure and temperature, and detonation waves were formed through deflagration-to-detonation transition (DDT) process in the smooth and straight channel in which no cross-sectional area change existed. The reaction wave in the small channels went through flame acceleration, detonation transition, and overdriven detonation before stably propagated along the chanel at a value lower than the Chapman-Jouguet velocity. As the channel size decreased from 1.2 mm to 0.6 mm, both DDT time and DDT distance reduced while the detonation velocity deficit increased. In the 0.8 mm channel, the propagation speed of detonation wave dropped after a certain distance after detonation transition, and then fluctuated around a new value. Low-speed detonation mode appeared when the channel size was 0.6 mm. Moreover, the detonation velocity deficit gradually increased with the decrease of equivalence ratio within the test range. Non-dimensional detonation velocities V/VCJ becomes invariant as non-dimensional number DH/λ is larger than 1.4. But the deficit is not only a function of DH/λ for near-limit conditions when the channel dimension approaches or becomes smaller than the cell size.

Original languageEnglish
StatePublished - 2017
Event11th Asia-Pacific Conference on Combustion, ASPACC 2017 - Sydney, Australia
Duration: 10 Dec 201714 Dec 2017

Conference

Conference11th Asia-Pacific Conference on Combustion, ASPACC 2017
Country/TerritoryAustralia
CitySydney
Period10/12/1714/12/17

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