TY - JOUR
T1 - Application of hemisphere radiation shields with temperature-dependent emissivity for reducing heat transfer between two concentric hemispheres
AU - Torabi, M.
AU - Aziz, A.
AU - Saedodin, S.
PY - 2012
Y1 - 2012
N2 - The radiation network method has been applied to calculate the net radiation heat transfer between two concentric hemispheres separated by two hemispherical radiation shields with temperature-dependent surface emissivities. Three different materials are chosen for radiation shields: aluminum oxide, silicon carbide, and tungsten. The reduction in heat transfer with shields depends not only on the surface characteristics of the two shields, but also on the locations of the shields. Three illustrative examples are presented to illustrate the effects of temperature dependent emissivities and shield locations on the percentage heat transfer reduction. The analysis can be used to study other cases as warranted. © 2012 Pleiades Publishing, Ltd.
AB - The radiation network method has been applied to calculate the net radiation heat transfer between two concentric hemispheres separated by two hemispherical radiation shields with temperature-dependent surface emissivities. Three different materials are chosen for radiation shields: aluminum oxide, silicon carbide, and tungsten. The reduction in heat transfer with shields depends not only on the surface characteristics of the two shields, but also on the locations of the shields. Three illustrative examples are presented to illustrate the effects of temperature dependent emissivities and shield locations on the percentage heat transfer reduction. The analysis can be used to study other cases as warranted. © 2012 Pleiades Publishing, Ltd.
KW - concentric hemispherical system
KW - locations of shields
KW - radiation network method
KW - radiation shields
KW - temperature-dependent surface emissivities
UR - http://www.scopus.com/inward/record.url?scp=84872286531&partnerID=8YFLogxK
UR - https://www.scopus.com/record/pubmetrics.uri?eid=2-s2.0-84872286531&origin=recordpage
U2 - 10.1134/S0869864312030134
DO - 10.1134/S0869864312030134
M3 - RGC 21 - Publication in refereed journal
SN - 0869-8643
VL - 19
SP - 481
EP - 488
JO - Thermophysics and Aeromechanics
JF - Thermophysics and Aeromechanics
IS - 3
ER -