2018
DOI: 10.4271/2018-01-0296
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Characterization of Hollow Cone Gas Jets in the Context of Direct Gas Injection in Internal Combustion Engines

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Cited by 21 publications
(13 citation statements)
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“…Due to higher than critical pressure ratios and varying cross sections, the flow within the nozzle reaches supersonic velocities. Previous simulations in Deshmukh et al 30 showed that the boundary layer is very thin in the nozzle and has a minor impact on the flow except at the exit, where flow separation occurs. Therefore, the viscous effects are neglected, and the Euler equations are considered for modeling the nozzle gap.…”
Section: Model Developmentmentioning
confidence: 98%
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“…Due to higher than critical pressure ratios and varying cross sections, the flow within the nozzle reaches supersonic velocities. Previous simulations in Deshmukh et al 30 showed that the boundary layer is very thin in the nozzle and has a minor impact on the flow except at the exit, where flow separation occurs. Therefore, the viscous effects are neglected, and the Euler equations are considered for modeling the nozzle gap.…”
Section: Model Developmentmentioning
confidence: 98%
“…A state-of-the-art compressible solver CHRIS (Compressible High-speed Reactive Solver) developed by Cascade Technologies Inc. is used for high-fidelity LES. 33 For details on the numerical schemes and setup information, the reader is referred to Deshmukh et al 30 The flow variables from the quasi-1-D model are compared with the flow variables on the centerline of the nozzle gap from the 3-D LES data. This comparison is valid because the wall boundary layer in 3-D LES is found to be thin due to the high-speed flow through the nozzle resulting in almost top-hat profiles.…”
Section: Model Developmentmentioning
confidence: 99%
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