2019
DOI: 10.1016/j.fuel.2019.04.030
|View full text |Cite|
|
Sign up to set email alerts
|

Promoting “adiabatic core” approximation in a rapid compression machine by an optimized creviced piston design

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1
1

Citation Types

2
20
0

Year Published

2020
2020
2024
2024

Publication Types

Select...
8

Relationship

2
6

Authors

Journals

citations
Cited by 33 publications
(22 citation statements)
references
References 40 publications
2
20
0
Order By: Relevance
“…Figure shows the evolution of the IDTs in terms of neat iso-octane as a function of the inverse of temperature in this work, along with the available results from other groups. ,, It can be seen that the IDTs are consistent with the ones obtained by other research teams, and this implies that the RCM apparatus in Orleans is able to yield reliable experimental data among the combustion community. Besides, the state-of-art work can extend the temperature range from 600 to 950 K. Similar to the other studies, the negative temperature coefficient (NTC) temperature range of iso-octane was well characterized between 700 and 800 K, though the IDTs in this work were longer than some of those in other groups at temperatures above 750 K. As for the first-stage IDTs, at a temperature range from 675 to 775 K, they exhibited a monotonic decrease trend which was also observed by other groups.…”
Section: Resultssupporting
confidence: 80%
“…Figure shows the evolution of the IDTs in terms of neat iso-octane as a function of the inverse of temperature in this work, along with the available results from other groups. ,, It can be seen that the IDTs are consistent with the ones obtained by other research teams, and this implies that the RCM apparatus in Orleans is able to yield reliable experimental data among the combustion community. Besides, the state-of-art work can extend the temperature range from 600 to 950 K. Similar to the other studies, the negative temperature coefficient (NTC) temperature range of iso-octane was well characterized between 700 and 800 K, though the IDTs in this work were longer than some of those in other groups at temperatures above 750 K. As for the first-stage IDTs, at a temperature range from 675 to 775 K, they exhibited a monotonic decrease trend which was also observed by other groups.…”
Section: Resultssupporting
confidence: 80%
“…To clearly illustrate the combustion process of RP-3 spray, some typical stages during the pressure trace, as shown in Figure 3, were extracted, as shown in Figure 4. Before the compression, no in-cylinder vortex was observed in the window, whereas the mixture was compressed by the piston, and vortexes appeared from the window boundary near the piston top and gathered around the central region, which was consistent with our previous simulations [26]. The gaseous mixture was pushed into the core region of the chamber or into the piston crevice due to the piston motion.…”
Section: Data Collection and Analysis Processingsupporting
confidence: 90%
“…This method was demonstrated to be effective through comparison with the measured results by Nasir and Farooq [33]. An optimized piston [26] with a suitable hydraulic system [34] was used to restrain the in-cylinder roll-up and ensure homogeneity. Additionally, gaseous mixtures consisting of oxygen, nitrogen, and argon with purities all over 99.99% were charged into the chamber before the fuel injection, which guaranteed that no chemical reactions would happen during the compression stroke and further improved the assumption accuracy.…”
Section: Data Collection and Analysis Processingmentioning
confidence: 99%
See 1 more Smart Citation
“…All the experiments regarding the ignition of C 2 H 6 /O 2 /Ar mixtures with or without NO 2 were conducted in a rapid compression machine (RCM), which has been elaborately described and validated in our previous publications. The facility has five components, namely, a high-pressure stainless tank, a hydraulic stopping mechanism, a pneumatic driving chamber, a compression chamber, and a combustion chamber.…”
Section: Methodsmentioning
confidence: 99%