Abstract
A substantial amount of research has recently focused on kinetically controlled combustion strategies such as reactivity-controlled compression ignition combustion. These strategies are promising methods to achieve high efficiency with near-zero NOx and soot emissions; however, despite promising results, very few attempts have been made to develop size-scaling relationships that would allow these results to be generalized to any engine design. Engine design is a long and arduous process that requires a substantial amount of experimental work. Consequently, it is of interest to develop scaling laws that allow results from one engine to be extrapolated to new designs. Several scaling laws have been proposed for diffusion combustion (i.e. mixing limited) that scale parameters such as liquid length and lift-off length. Such parameters have been deemed unimportant for highly premixed low-temperature combustion strategies; thus, a new methodology is needed. The present effort uses a combination of detailed computational fluid dynamics simulations and engine experiments in two engines with different bore sizes to develop a new engine size–scaling methodology for low-temperature kinetically controlled combustion strategies. The effects of pressure, temperature, and turbulence timescales are explored in order to replicate the large-bore engine performance in a small-bore engine. A size-scaling relationship based on the ignition timescale is proposed and used to generalize the results to an arbitrary bore size and fuel combination.
Original language | English |
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Pages (from-to) | 927-947 |
Number of pages | 21 |
Journal | International Journal of Engine Research |
Volume | 21 |
Issue number | 6 |
DOIs | |
State | Published - Aug 1 2020 |
Externally published | Yes |
Funding
The authors would like to thank Convergent Sciences for providing licenses for CONVERGE, and CET for providing licenses for Ensight. The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: Financial support from the Office of Naval Research (contract N000141410695) with program managers Donald Hoffman and Harold Scott Coombe.
Funders | Funder number |
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Office of Naval Research | N000141410695 |
Commonwealth Education Trust |
Keywords
- Fuel reforming
- engine scaling
- low-temperature combustion
- reactivity-controlled compression ignition combustion
- syngas