Abstract
Natural gas, a fuel abundant in nature, cannot be used by itself in conventional diesel engines because of its low cetane number. However, it can be used as the primary fuel with ignition by a pilot diesel spray. This is called dual-fuelling. The gas may be introduced either into the inlet manifold or, preferably, directly into the cylinder where it is injected as a short duration, intermittent, sonic jet. For accurate delivery in the latter case, a constant flow-rate from the injector is required into the constantly varying pressure in the cylinder. Thus, a sonic (choked) jet is required which is generally highly under-expanded. Immediately at the nozzle exit, a shock structure develops which can provide essential information about the downstream flow. This shock structure, generally referred to as a “barrel” shock, provides a key to understanding the full injection process. It is examined both experimentally and numerically in this paper.
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Abbreviations
- A :
-
Area (m2)
- CFD:
-
Computational fluid dynamics
- CI:
-
Compression-ignition
- D :
-
Diameter (m)
- DF:
-
Dual-fuel
- HPCR:
-
High-pressure common-rail
- M :
-
Mach number
- NG:
-
Natural gas
- SI:
-
Spark-ignition
- SOI:
-
Start of injection
- UHC:
-
Unburned hydrocarbons
- V :
-
Volume (m3)
- x :
-
Distance from the nozzle (m)
- ρ :
-
Density (kg/m3)
- γ :
-
Ratio of specific heats
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Communicated by B.W. Skews.
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White, T.R., Milton, B.E. Shock wave calibration of under-expanded natural gas fuel jets. Shock Waves 18, 353–364 (2008). https://doi.org/10.1007/s00193-008-0158-6
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DOI: https://doi.org/10.1007/s00193-008-0158-6