Numerical and experimental analysis of thermal-flow characteristics in a pyrolysis reactor of a gas scrubber designed based on similitude theory

2020 ◽  
Vol 70 (5) ◽  
pp. 532-543
Author(s):  
Jonghyuk Yoon ◽  
Youngbae Kim ◽  
Hyoungwoon Song
Author(s):  
Shashank R Chaurasia ◽  
RM Sarviya

An experimental analysis has been carried out to investigate the thermal and friction factor characteristics of fluid flow in a tube with double strip helical screw tape (DS-HST) inserts with different values of twist ratio and compared with single strip helical screw tape inserts and plain tube. Water is used as a working fluid at different flow rates with constant heat flux conditions. CFD analysis is also carried out to visualize thermal and fluid flow characteristics of fluid flow in tube with inserts. Experimental results have showed that Nusselt number and friction factor have attained excellent enhancement with double strip helical screw tape inserts in the range of flow rates than single strip helical screw tape inserts at the value of twist ratio 1.5. Correlation is also developed for Nusselt number with a range of Reynolds number, twist ratio and number of strips. Moreover, the performance ratio has attained maximum value at twist ratio of 2.5 with high values of flow rate. It is concluded that DS-HST is able to attain enhancement in the efficiency of heat exchanger, causing a reduction in size for thermal applications.


Author(s):  
Moon-Young Cho ◽  
Hyeon-Seok Seo ◽  
Youn-Jea Kim

In this study, the effect of a row of double-jet film-cooling hole configurations on the thermal-flow characteristics of gas turbine blades was examined. To investigate the effect of the interference of anti-kidney vortices, the ratios of the pitch distance and hole diameter (P/d=5, 6.25, 8.333) were considered with two different compound angles (λ=0°, 4°). The film cooling performance and the generated losses were studied. Then, the relevant mechanisms were identified and explained. A numerical study was performed using ANSYS CFX 14.5 with the shear stress transport (SST) turbulent model. The blowing ratio was kept at a constant value of M=1.5. The film cooling effectiveness and temperature distribution are graphically depicted with various geometrical configurations.


Author(s):  
Tao Wang ◽  
Maosheng Wang ◽  
Youliang Su ◽  
Song Mu ◽  
Kai Jing ◽  
...  

2020 ◽  
Vol 85 ◽  
pp. 108624
Author(s):  
F. Felis ◽  
S. Tomas ◽  
A. Vallet ◽  
M. Amielh ◽  
F. Anselmet

1993 ◽  
Author(s):  
Kenji Date ◽  
Hiroyuki Nobechi ◽  
Hiroyuki Kano ◽  
Masaaki Kato ◽  
Takio Oya

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