scholarly journals Experimental and theoretical investigations on heat transfer of strongly heated turbulent gas flow in an annular duct.

1990 ◽  
Vol 56 (521) ◽  
pp. 122-128
Author(s):  
Sadao FUJII ◽  
Norio AKINO ◽  
Makoto HISHIDA ◽  
Hiroshi KAWAMURA ◽  
Konomo SANOKAWA
Author(s):  
Kyohei Isobe ◽  
Chungpyo Hong ◽  
Yutaka Asako ◽  
Ichiro Ueno

Numerical simulations were performed to obtain for heat transfer characteristics of turbulent gas flow in micro-tubes with constant wall temperature. The numerical methodology was based on Arbitrary-Lagrangian-Eulerinan (ALE) method to solve compressible momentum and energy equations. The Lam-Bremhorst Low-Reynolds number turbulence model was employed to evaluate eddy viscosity coefficient and turbulence energy. The tube diameter ranges from 100 μm to 400 μm and the aspect ratio of the tube diameter and the length is fixed at 200. The stagnation temperature is fixed at 300 K and the computations were done for wall temperature, which ranges from 305 K to 350 K. The stagnation pressure was chosen in such a way that the flow is in turbulent flow regime. The obtained Reynolds number ranges widely up to 10081 and the Mach number at the outlet ranges from 0.1 to 0.9. The heat transfer rates obtained by the present study are higher than those of the incompressible flow. This is due to the additional heat transfer near the micro-tube outlet caused by the energy conversion into kinetic energy.


1969 ◽  
Vol 16 (4) ◽  
pp. 400-403 ◽  
Author(s):  
V. M. Buznik ◽  
Z. I. Geller ◽  
A. K. Pimenov

2010 ◽  
Vol 2010 (0) ◽  
pp. 253-254
Author(s):  
Kyohei ISOBE ◽  
Chungpyo HONG ◽  
Ichiro UENO ◽  
Yutaka ASAKO ◽  
Koichi SUZUKI

Author(s):  
Sadao FUJII ◽  
Norio AKINO ◽  
Makoto HISHIDA ◽  
Hiroshi KAWAMURA ◽  
Konomo SANOKAWA

1974 ◽  
Author(s):  
A. AMBRAZEVICIUS ◽  
A. ZUKAUSKAS ◽  
P. VALATKEVICIUS ◽  
R. KEZELIS

Author(s):  
Chungpyo Hong ◽  
Kyohei Isobe ◽  
Yutaka Asako ◽  
Ichiro Ueno

This paper describes experimental results on total temperature measurement to obtain heat transfer characteristics of turbulent gas flow in a microtube with constant wall temperature. The experiments were performed for nitrogen gas flow through a microtube of 354 μm in diameter with 100 mm in length. The wall temperature was maintained at 310 K, 330 K, and 350 K by circulating water around the microtube, respectively. The stagnation pressure was chosen in such a way that the exit Mach number ranges from 0.1 to 1.0. In order to obtain heat transfer rate of turbulent gas flow through a micro-tube, the total temperatures of gas flowing out of a microtube exit were measured with the set of total temperature measurement attached to micro stage with position fine adjustment. The numerical computations based on the Arbitrary - Langrangian - Eulerian (ALE) method were also performed for the turbulent gas flow with the same conditions of the experiments. The results were in excellent agreement.


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