TY - JOUR
T1 - Numerical Analysis of Thermal Plasma Flow in a Pipe
AU - Kobayashi, Masakazu
AU - Honda, Takuya
AU - Kanzawa, Atsushi
N1 - Copyright:
Copyright 2017 Elsevier B.V., All rights reserved.
PY - 1983/1
Y1 - 1983/1
N2 - Numerical calculations were carried out to investigate the behavior of the thermal plasma flow in a water-cooled pipe, assuming three states: thermal equilibrium, frozen and approximately real state. From these results, it was found that the velocity and energy profiles are different from an ordinary pipe flow and vary characteristically depending on the state in a pipe and the initial condition. For example, center-line velocity increases and then decreases, bulk temperature and total enthalpy do not change in a similar manner, and the pressure decreases and then increases. With regard to heat flux to the pipe wall, the Nusselt number, Nu, was calculated according to the ordinary method and this result is discussed.
AB - Numerical calculations were carried out to investigate the behavior of the thermal plasma flow in a water-cooled pipe, assuming three states: thermal equilibrium, frozen and approximately real state. From these results, it was found that the velocity and energy profiles are different from an ordinary pipe flow and vary characteristically depending on the state in a pipe and the initial condition. For example, center-line velocity increases and then decreases, bulk temperature and total enthalpy do not change in a similar manner, and the pressure decreases and then increases. With regard to heat flux to the pipe wall, the Nusselt number, Nu, was calculated according to the ordinary method and this result is discussed.
UR - http://www.scopus.com/inward/record.url?scp=85010130922&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85010130922&partnerID=8YFLogxK
U2 - 10.1252/kakoronbunshu.9.622
DO - 10.1252/kakoronbunshu.9.622
M3 - Article
AN - SCOPUS:85010130922
SN - 0386-216X
VL - 9
SP - 622
EP - 627
JO - Kagaku Kogaku Ronbunshu
JF - Kagaku Kogaku Ronbunshu
IS - 6
ER -