Internal recirculation flow structure in vertical upflow gas-solids suspensions part I. A core-annulus model

1996 ◽  
Vol 22 ◽  
pp. 144
Author(s):  
D Bai
1995 ◽  
Vol 85 (2) ◽  
pp. 179-188 ◽  
Author(s):  
Dingrong Bai ◽  
Jing-Xu Zhu ◽  
Yong Jin ◽  
Zhiquing Yu

2014 ◽  
Vol 656 ◽  
pp. 53-63 ◽  
Author(s):  
Krishna Murari Pandey ◽  
Sukanta Roga

This paper presents a numerical analysis of the inlet-combustor interaction and flow structure through a scramjet engine at a flight Mach 6 with cavity based injection. Fuel is injected at supersonic speed of Mach 2 through a cavity based injector. These numerical simulations are aimed to study the flow structure, supersonic mixing and combustion for cavity based injection. For the reacting cases, the shock wave pattern is modified which is due to the strong heat release during combustion process. The shock structure and combustion phenomenon are not only affected by the geometry but also by the flight Mach number and the trajectory. The inlet-combustor interaction is studied with a fix location of cavity based injection. Cavity is of interest because recirculation flow in cavity would provide a stable flame holding while enhancing the rate of mixing or combustion. The cavity effect is discussed from a view point of mixing and combustion efficiency.


2011 ◽  
Vol 268-270 ◽  
pp. 494-500
Author(s):  
Jai Houng Leu

This study applied three-dimension numerical combustion simulation method to design the specifications of a low heating value (LHV) fuel combustor. According to the discussion on design parameter system, quantity of main jets is the governing factor for flame stabilization of the primary combustor zone. Combustor outlet temperature factor improves with increase of load, and can be reduced to 0.33 under full load. However, load increase may slightly change recirculation flow structure and weaken flame stabilization. The findings showed that the combustion strength of near-field area greatly increased, and the recirculation flow structure center moved to the liner well when combustor used propane as fuel. This also caused deterioration of temperature factor.


1995 ◽  
Vol 85 (2) ◽  
pp. 171-177 ◽  
Author(s):  
Dingrong Bai ◽  
Jing-Xu Zhu ◽  
Yong Jin ◽  
Zhiqing Yu

2016 ◽  
Vol 47 (4) ◽  
pp. 359-382 ◽  
Author(s):  
Nabil Kharoua ◽  
Lyes Khezzar ◽  
Zoubir Nemouchi

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