Comparison of different lobe-injectors on fuel mixing characteristics of single jet at the supersonic combustion chamber

2021 ◽  
pp. 107193
Author(s):  
Guangli Fan ◽  
Hassan Abdulwahab Anjal ◽  
Raed Qahiti ◽  
Nidal H. Abu-Hamdeh ◽  
Abdullah M. Abusorrah ◽  
...  
2021 ◽  
pp. 107299
Author(s):  
Qingji Tian ◽  
Yi-Peng Xu ◽  
Nidal H. Abu-Hamdeh ◽  
Abdullah M. Abusorrah ◽  
Mahmoud M. Selim

2021 ◽  
pp. 106841
Author(s):  
Yu Jiang ◽  
Masoud Hajivand ◽  
Hosein Sadeghi ◽  
M. Barzegar Gerdroodbary ◽  
Zhixiong Li

Author(s):  
Tingting Jing ◽  
Zhen Xu ◽  
Jiachen Xu ◽  
Fei Qin ◽  
Guoqiang He ◽  
...  

2020 ◽  
Vol 45 (15) ◽  
pp. 9077-9087 ◽  
Author(s):  
Zhixiong Li ◽  
Tran Dinh Manh ◽  
M. Barzegar Gerdroodbary ◽  
Nguyen Dang Nam ◽  
R. Moradi ◽  
...  

2020 ◽  
Vol 45 (51) ◽  
pp. 27828-27836 ◽  
Author(s):  
Yu Jiang ◽  
Amin Poozesh ◽  
Seyed Maziar Marashi ◽  
R. Moradi ◽  
M. Barzegar Gerdroodbary ◽  
...  

Author(s):  
Peter L. Woodfield ◽  
Kazuya Tatsumi ◽  
Kazuyoshi Nakabe ◽  
Kenjiro Suzuki

A three-dimensional unstructured finite-volume method is used to investigate laminar flow characteristics of a miniature chamber with a possible application to micro gas turbine combustor design. The chamber is cylindrical in shape and 20mm in diameter with the fuel stream entering via a single jet in the center of one end of the can. Oxidizer jets are generated by a circular baffle plate having six holes surrounding the fuel jet. Attention is given to the effect of the inlet conditions on the flow structure and mixing pattern inside the chamber. Computations are carried out with the calculation domain inlet being positioned at two different locations; (1) at the immediate entrance to the combustion chamber (2) one combustor diameter upstream of the baffle plate. Numerous inlet conditions are considered including ‘top-hat’, fully-developed, swirling, an annular backward facing step and some asymmetrically skewed profiles. The baffle plate is shown to have a significant smoothing effect on the inlet conditions for a Reynolds number of 100.


1998 ◽  
Vol 33 (5) ◽  
pp. 637-644 ◽  
Author(s):  
A. N. Kraiko ◽  
V. E. Makarov ◽  
N. I. Tillyayeya

Author(s):  
Doohyun Kim ◽  
Angela Violi ◽  
André Boehman

Increased Particulate Matter (PM) emissions from Gasoline Direct Injection (GDI) engines compared to conventional Port Fuel Injection (PFI) engines have been raising concerns because of the PM’s detrimental health effects and the stringent emissions regulations. One of the widely accepted hypotheses is that local rich pockets inside the combustion chamber are the primary reason for the increased PM emissions. In this paper, we investigate the effects of injection strategies on the charge composition and local thermodynamic conditions of a light duty GDI engine, and determine their impact on PM emissions. The operation of a 1.6L GDI engine is simulated using a 3-D Computational Fluid Dynamics (CFD) code. Combustion characteristics of a 3-component gasoline surrogate (n-heptane/iso-octane/toluene) are analyzed and the effects of injection timing (300° vs 240° vs 180° BTDC) and injected fuel mass (globally stoichiometric vs fuel rich) are explored at 2000 rpm, 9.5 bar BMEP condition, focusing on the homogeneity of the charge and the formation of the gaseous species that are soot precursors. The results indicate that when the physical time for air/fuel mixing is not long enough, fuel-rich pockets are present until combustion occurs, where high concentrations of soot precursors are found, such as acetylene and pyrene. In addition, simulation results indicate that the location of wetted surface as well as the in-cylinder flow structure induced by the fuel jet hitting the piston bowl is significantly influenced by varying the injection timing, which affects subsequent air/fuel mixing. When the injected fuel mass is increased, the equivalence ratio distribution inside the combustion chamber shifts toward fuel-rich side, generating more mixtures with Φ > 1.5, where formation of acetylene and pyrene are favored.


2001 ◽  
Vol 2001.76 (0) ◽  
pp. _2-1_-_2-2_
Author(s):  
Kazuhide IWASA ◽  
Daisuke SEGAWA ◽  
Hiroshi ENOMOTO ◽  
Toshikazu KADOTA

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