Published 1995 | Version v1
Miscellaneous Open

Effect of turbulence on deflagration to detonation transition

  • 1. Atomic Energy of Canada Ltd., Pinawa, MB (Canada). Whiteshell Labs.
  • 2. Manitoba Univ., Winnipeg, MB (Canada). Dept. of Mechanical Engineering

Description

The interaction of a turbulent jet and an expanding flame kernel was examined using spark-schlieren photography and piezoelectric pressure transducers. Experiments were performed in a 9 by 9 cm, 4-m-long shock channel. Results show that an expanding flame kernel can be locally, or partially, quenched by flame stretching. The mixing of the hot combustion products, containing reactive species, with the unburnt gas in the turbulent flame-jet, created pockets of sensitized mixture. The subsequent re-ignition of the sensitized mixture could result in a local explosion. In a number of experiments the blast waves produced in the local explosion developed into detonation waves. A local explosion occurred only if there was partial quenching of the flame kernel. Partial quenching occurs when the Karlovitz-Kovaszney factor approaches unity and, therefore, it is possible to establish a set of conditions in terms of turbulent parameters for the transition to detonation. (author). 16 refs., 13 figs

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Part of:
CNS proceedings of the 16. annual conference, volume I and II

Additional details

Publishing Information

Imprint Title
CNS proceedings of the 16. annual conference, volume I and II
Imprint Pagination
2 v.
Journal Page Range
(v.1) [16 p.].
Report number
INIS-CA--0053

Conference

Title
16. Annual conference of the Canadian Nuclear Society.
Dates
4-7 Jun 1995.
Place
Saskatoon, SK (Canada).

Optional Information