2016
DOI: 10.1016/j.fuel.2016.06.112
|View full text |Cite
|
Sign up to set email alerts
|

Ultra high speed investigation of gaseous jet injected by a single-hole injector and proposing of an analytical method for pressure loss prediction during transient injection

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

0
7
0

Year Published

2017
2017
2022
2022

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 23 publications
(7 citation statements)
references
References 25 publications
0
7
0
Order By: Relevance
“…The validity of this model has been demonstrated for highly underexpanded jets with pressure ratio of up to 70, unaffected by the barrel-shaped shock. This model, described by Equations (4) and (5) [110,111], assumes a constant momentum discharge rate and density during the injection, as well as self-similar jet velocity and mixing distribution. Since the underexpanded jet flow is choked, the nozzle exit velocity (subscript e) is assumed to be the sonic speed [112].…”
Section: Axial Jet Penetrationmentioning
confidence: 99%
See 1 more Smart Citation
“…The validity of this model has been demonstrated for highly underexpanded jets with pressure ratio of up to 70, unaffected by the barrel-shaped shock. This model, described by Equations (4) and (5) [110,111], assumes a constant momentum discharge rate and density during the injection, as well as self-similar jet velocity and mixing distribution. Since the underexpanded jet flow is choked, the nozzle exit velocity (subscript e) is assumed to be the sonic speed [112].…”
Section: Axial Jet Penetrationmentioning
confidence: 99%
“…In reality, the effective pressure (P eff ) at the nozzle exit is less than the fuel supply reservoir pressure due to the high compressibility of gas flow [113], which is not considered in Equation (4). An estimation of the effective pressure depending on the reservoir pressure, ambient pressure and other gas properties was developed by Hajialimohammadi et al [111] based on the shock tube diaphragm rupture process as described by Equation (7). The effective pressure ratio to the ambient pressure (P eff /P a ) in Equation (7) can be approximated using the Newton-Raphson method.…”
Section: Axial Jet Penetrationmentioning
confidence: 99%
“…The effects of this barrel-shaped pattern on the downstream flow can be represented by employing the pseudo-diameter concept (Ouellette and Hill 2000). The pressure drop caused by the expansion wave travelling upstream the nozzle (towards the high-pressure side) can be estimated by using the shock tube theory, as reported in Hajialimohammadi et al (2016).…”
Section: Gas Injection Modelmentioning
confidence: 99%
“…This study aims at developing a CFD model to sufficiently represent the processes of the closed cycle of a marine two-stroke engine with direct gaseous fuel injection. To address the previous studies limitations discussed above, the pseudo-diameter concept (Ouellette and Hill 2000) and the one-dimensional shock tube theory (Hajialimohammadi et al 2016) are combined to accurately evaluate the gas jet penetration and the air entrainment. In addition, a novel approach for modelling the gas admission in the engine combustion chamber is developed by appropriately calculating the corresponding source terms in the governing equations.…”
Section: Introductionmentioning
confidence: 99%
“…As the high-pressure gas is injected into the engine combustion chamber, the underexpanded flow near the gas nozzle and the expansion fan navigating toward the high-pressure side inside the gas nozzle are observed, which significantly affects the gas injection and cause entrainment with the ambient mixture. 17,18 Herein, the pseudo-diameter concept 17 and the one-dimensional (1D) shock tube theory are employed to evaluate such effects, as proposed in Hajialimohammadi et al 18 The normal gas injection velocity and the pseudo-diameter are calculated by the following formulas…”
Section: Mathematic Modelsmentioning
confidence: 99%