Report
Combustion characteristics in the transition region of liquid fuel sprays
01 Jan 1986
Abstract
A number of important effects have been observed in the droplet size transition region in spray combustion systems. In this region, where the mechanism of flame propagation is transformed from diffusive to premixed dominated combustion, the following effects have been observed: (1) maxima in burning velocity; (2) extension of flammability limits; (3) minima in ignition energy; and (4) minima in NOx formation. A monodisperse aerosol generator has been used to form and deliver a well controlled liquid fuel spray to the combustion test section where measurements of ignition energy have been made. The ignition studies were performed on monodisperse n-heptane sprays at atmospheric pressure over a range of equivalence ratios and droplet diameters. A capacitive discharge spark ignition system was used as the ignition source, providing independent control of spark energy and duration. Preliminary measurements were made to optimize spark duration and spark gap, optimum conditions being those at which the maximum frequency or probability of ignition was observed. Using the optimum electrode spacing and spark duration, the frequency of ignition was determined as a function of spark energy for three overall equivalence ratios (0.6, 0.8, and 1.0) and for initial droplet diameters of 25, 40, 50, 60, and 70 micro m.
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Details
- Title
- Combustion characteristics in the transition region of liquid fuel sprays
- Creators
- N. P. Cernansky - Drexel UniversityI. Namer - Drexel UniversityR. J. Tidona - Drexel University
- Publisher
- National Aeronautics and Space Administration
- Resource Type
- Report
- Language
- English
- Academic Unit
- Mechanical Engineering and Mechanics
- Identifiers
- 991020202227804721