Gas Mixing in Circulating Fluidized Beds with Secondary Air Injection

2004 ◽  
Vol 82 (8) ◽  
pp. 979-992 ◽  
Author(s):  
M. Koksal ◽  
F. Hamdullahpur
2000 ◽  
Vol 177 (1) ◽  
pp. 31-47 ◽  
Author(s):  
YONG KANG ◽  
PYUNG S. SONG ◽  
JONG S. YUN ◽  
YI Y. JEONG ◽  
SANG D. KIM

RSC Advances ◽  
2016 ◽  
Vol 6 (43) ◽  
pp. 36642-36655 ◽  
Author(s):  
Rong Zhang ◽  
Zhenhua Hao ◽  
Zhiyu Wang ◽  
Xiaodong Huo ◽  
Junguo Li ◽  
...  

This paper investigated the distribution of secondary air after injection into a multi-stage conversion fluidized bed (MFB) cold model.


2019 ◽  
pp. 913-922
Author(s):  
Sagar Namdev Khurd ◽  
U. B. Andh ◽  
S. V. Kulkarni ◽  
Sandeep S. Wangikar ◽  
P. P. Kulkarni

2000 ◽  
Vol 16 ◽  
pp. 427-432
Author(s):  
Yoshihito SUZUKI ◽  
Yasumasa KUROSAWA ◽  
Minoru OCHIAI ◽  
Shigekatsu ENDO

2017 ◽  
Vol 135 ◽  
pp. 00014
Author(s):  
Mohd Faizal Mohideen Batcha ◽  
Sulastri Sabudin ◽  
Jamal Hazri Zakaria

1998 ◽  
Vol 120 (2) ◽  
pp. 342-347 ◽  
Author(s):  
B. A. Jubran ◽  
M. S. Al-Haroun

This paper reports an experimental investigation to study the effects of using various designs of secondary air injection hole arrangements on the heat transfer coefficient and the pressure drop characteristics of an array of rectangular modules at different values of free-stream Reynolds numbers in the range 8 × 103 to 2 × 104. The arrangement used is either one staggered row of simple holes or one row of compound injection holes. The pitch distances between the injection holes, as well as the injection angles, were varied in both the streamwise and spanwise directions. Generally, the presence of secondary air through the injection hole arrangement can give up to 54 percent heat transfer enhancement just downstream of the injection holes. The amount of heat transfer enhancement and pressure drop across the electronic modules is very much dependent on the design of the injection holes. The simple angle injection hole arrangement tends to give a better heat transfer enhancement and less pressure drop than the compound angle holes.


1991 ◽  
Vol 113 (3) ◽  
pp. 375-383 ◽  
Author(s):  
A. Yamamoto ◽  
Y. Kondo ◽  
R. Murao

In order to understand overall performance and internal flows of air-cooled turbine blade rows, flows in a model linear cascade were surveyed with secondary air injection from various locations of the blade surfaces. The secondary air interacted with the cascade passage vortices and changed the loss distribution significantly. The cascade overall loss decreased when the air was injected along the mainstream and increased when the air was injected against the mainstream from some locations of the blade leading edge. Effects on overall kinetic energy of the secondary flows and on the cascade outlet flow angle were also discussed in this paper.


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