Development and verification of RP-3 aviation kerosene surrogate fuel models using a genetic algorithm

Fuel ◽  
2022 ◽  
Vol 312 ◽  
pp. 122853
Author(s):  
Zhiqing Yu ◽  
Shengli Wei ◽  
Chengcheng Wu ◽  
Lirong Wu ◽  
Linxiao Sun ◽  
...  
Author(s):  
Wenjin Qin ◽  
Dengbiao Lu ◽  
Lihui Xu

Abstract In this research, n-dodecane and JW are selected as single and multi-component surrogate fuel of aviation kerosene to study the Jet-A spray combustion characteristics. The spray combustion phenomena are simulated using large eddy simulation coupled with detailed chemical reaction mechanism. Proper orthogonal decomposition method is applied to analyze the flow field characteristics, and the instantaneous velocity field are decomposed into four parts, namely the mean field, coherent field, transition field and turbulent field, respectively. The four subfields have their own characteristics. In terms of different fuels, JW has a higher intensity of coherent structures and local vortices than n-dodecane, which promotes the fuel-air mixing and improves the combustion characteristics, and the soot formation is significantly reduced. In addition, with the increase of initial temperature, the combustion is more intense, the ignition delay time is advanced, the flame lift-off length is reduced, and soot formation is increased accordingly.


Fuel ◽  
2016 ◽  
Vol 181 ◽  
pp. 120-130 ◽  
Author(s):  
Hiew Mun Poon ◽  
Kar Mun Pang ◽  
Hoon Kiat Ng ◽  
Suyin Gan ◽  
Jesper Schramm

Fuel ◽  
2016 ◽  
Vol 180 ◽  
pp. 433-441 ◽  
Author(s):  
Hiew Mun Poon ◽  
Kar Mun Pang ◽  
Hoon Kiat Ng ◽  
Suyin Gan ◽  
Jesper Schramm

2021 ◽  
Vol 226 ◽  
pp. 229-242 ◽  
Author(s):  
Yingtao Wu ◽  
Snehasish Panigrahy ◽  
Amrit B. Sahu ◽  
Chaimae Bariki ◽  
Joachim Beeckmann ◽  
...  

2019 ◽  
Vol 35 (3) ◽  
pp. 645-651 ◽  
Author(s):  
Bei-Jing Zhong ◽  
Hui-Sheng Peng

2016 ◽  
Vol 30 (12) ◽  
pp. 10847-10857 ◽  
Author(s):  
Yingwen Yan ◽  
Yunpeng Liu ◽  
Dong Di ◽  
Chao Dai ◽  
Jinghua Li

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