TREATMENT OF DISCONTINUOUS THERMAL-CONDUCTIVITY IN CONTROL-VOLUME SOLUTIONS OF PHASE-CHANGE PROBLEMS

被引:48
作者
VOLLER, VR
SWAMINATHAN, CR
机构
[1] University of Minnesota, Minneapolis, MN
关键词
D O I
10.1080/10407799308955887
中图分类号
O414.1 [热力学];
学科分类号
摘要
Phase-change problems often involve discontinuities in the thermal properties at the phase-change boundary. This feature needs to be handled carefully when seeking a numerical solution based on a fixed space grid. Of particular concern are discontinuities in the thermal conductivity. In the context of a control-volume finite-difference solution, the requirement is an appropriate approximation of the conductivity values at the control-volume interfaces. In this article, using the Kirchhoff transformation, for the interface conductivity is developed. The approach is tested on a range of one and two-dimensional, steady and transient phase-change problems. In addition, a discussion on the extension of the approach to finite-element schemes is included.
引用
收藏
页码:161 / 180
页数:20
相关论文
共 13 条
[1]   ON THE PERFORMANCE OF THE ENTHALPY METHOD [J].
BELL, GE .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1982, 25 (04) :587-589
[2]  
Comini G., 1974, International Journal for Numerical Methods in Engineering, V8, P613, DOI 10.1002/nme.1620080314
[3]  
Crank J., 1984, FREE MOVING BOUNDARY
[4]   AN ENTHALPY FORMULATION FOR PHASE-CHANGE PROBLEMS WITH A LARGE THERMAL-DIFFUSIVITY JUMP ACROSS THE INTERFACE [J].
LEE, SL ;
TZONG, RY .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1991, 34 (06) :1491-1502
[5]  
LEMMON EC, 1979, NUMERICAL METHODS TH, P149
[6]   FINITE-ELEMENT SIMULATION OF SOLIDIFICATION PROBLEMS [J].
LEWIS, RW ;
ROBERTS, PM .
APPLIED SCIENTIFIC RESEARCH, 1987, 44 (1-2) :61-92
[7]  
OLSSON ED, 1990, JUN AIAA ASME THERM
[8]  
Patankar S.V., 2018, NUMERICAL HEAT TRANS
[9]   THE EFFECT OF LATENT HEAT ON NUMERICAL SOLUTIONS OF THE HEAT FLOW EQUATION [J].
PRICE, PH ;
SLACK, MR .
BRITISH JOURNAL OF APPLIED PHYSICS, 1954, 5 (AUG) :285-287
[10]  
SIMARD G, 1989, 2ND PHOENICS US C DU