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Secondary effects in combustion instabilities leading to flashbackThe secondary effects in turbulent combustion instabilities leading to flashback are investigated, including those due to buoyancy and contraction at the combustor outlet. Experiments were conducted in an oblong, rectangular cross-section combustion tunnel, where the effects of a bluff-body flames holder were generated by a rear-facing step behind a streamlined inlet nozzle. The results of experiments leading to flashback with the step mounted at the bottom of the combustion chamber were compared to those of experiments in which it was located at the top. Irrespective of the flow obstructions introduced downstream, the critical equivalence ratio for flashback was consistently lower with the step at the bottom, indicating that buoyancy was enhancing the growth of the recirculation zone that pushed the flame upstream and caused flashback. The contraction at the end of the combustion chamber had a promoting influence on the process of vortex pairing, re-enforcing the influence of the trailing vortices over that of the recirculation vortex system, and thereby curbing the tendency to flashback. Provided that the flow velocity was low, however, the characteristic features of combustion instabilities leading to flashback in the absence of contraction could still be established in its presence.
Document ID
19820034211
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vaneveld, L.
(California Univ. Berkeley, CA, United States)
Hom, K.
(California Univ. Berkeley, CA, United States)
Oppenheim, A. K.
(California, University Berkeley, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA PAPER 82-0037
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A17746
Funding Number(s)
CONTRACT_GRANT: NSG-3227
CONTRACT_GRANT: W-7405-ENG-48
Distribution Limits
Public
Copyright
Other

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