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Development of a simplified n-heptane/methane model for high-pressure direct-injection natural gas marine engines

Frontiers in Energy 2021年第2期15卷 405-420页

作者： Jingrui LI Haifeng LIU Xinlei LIU Ying YE Hu WANG Xinyan WANG Hua ZHAO Mingfa YAO State Key Laboratory of Engines Tianjin UniversityTianjin 300072China Clean combustion Research Center King Abdullah University of Science and TechnologyThuwal 23955-6900Saudi Arabia Brunel University London Kingston LaneUxbridgeMiddlesex UB83PHUK

High-pressure direct-injection (HPDI) of natu- ral gas is one of the most promising solutions for future ship engines, in which the combustion process is mainly controlled by the chemical kinetics. However, the employment of detailed chemical models for the multi-dimensional combustion simulation is significantly expensive due to the large scale of the marine engine. In the present paper, a reduced n-heptane/methane model consisting of 35-step reactions was constructed using multiple reduction approaches. Then this model was further reduced to include only 27 reactions by utilizing the HyChem (Hybrid Chemistry) method. An overall good agreement with the experimentally measured ignition delay data of both n-heptane and methane for these two reduced models was achieved and reasonable predictions for the measured laminar flame speeds were obtained for the 35-step model. But the 27-step model cannot predict the laminar flame speed very well. In addition, these two reduced models were both able to reproduce the experimentally measured in-cylinder pressure and heat release rate profiles for a HPDI natural gas marine engine, the highest error of predicted combustion phase being 6.5%. However, the engine-out CO emission was over-predicted and the highest error of predicted NOx emission was less than 12.9%. The predicted distributions of temperature and equivalence ratio by the 35-step and 27-step models are similar to those of the 334-step model. However, the predicted distributions of OH and CH2O are significantly different from those of the 334-step model. In short, the reduced chemical kinetic models developed provide a high-efficient and dependable method to simulate the characteristics of combustion and emissions in HPDI natural gas marine engines.

关键词： high-pressure direct-injection natural gas chemical kinetics combustion modelling marine engine

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Numerical simulation of a hydrocarbon fuelled valveless pulsejet

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Propulsion and Power Research 2014年第2期3卷 90-95页

作者： Joseph Kalyan Raj Isac Logu Mohanraj Enumula Srikar Sai Vijay Kumar Kannan CD-adapco India Private Limited BangaloreKarnataka 560066India Park College of Engineering and Technology CoimbatoreTamilnadu 641659India

Jet propulsion technology has been limited to being identified largely with turbojets and turbo-machinery driven jet *** late there has been a renewed interest in pulsejet technology and it has once again caught the imagination of *** specific characteristics of the pulsejet,such as easy scalability,absence of moving parts,reduced combustion temperatures;lower NOX formation and the like make it possess varied capabilities for use in the field of jet propulsion and the most viable option for small-scale jet *** the current work,a numerical analysis encompassing feasibility and validation of a valveless pulsejet engine was attempted using CD-adapco's STAR-CCM+CFD *** to lack of comprehensive established mathematical laws to govern the working of a pulsejet,most experimental work being performed is done by trial and *** necessitates in-depth computational studies in order to shed more light on the understanding of valveless *** results have been encouraging and in agreement with observed experimental conclusions such as,i)changes in dimensions affect the working of a pulsejet,ii)presence of a flare enhances the working of a pulsejet,and the close agreement in the frequency of *** continuous study,an optimum initial condition was achieved which enabled the pulsejet to begin operation even before 0.05 s,thereby greatly reducing computational costs if a higher time-scale were to be used.

关键词： Pulsejet Pulsed-combustion Jet engines Computational fluid dynamics Eddy-break up model combustion modelling Propulsion STAR-CCM+

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