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从热力学理论和热力学模型两个方面综述了剪切对聚合物共混体系相行为的影响.剪切对聚合物共混体系相行为影响的理论研究中,出现了众多的热力学理论模型,包括Wolf理论模型、Onuki理论模型、Lyngaae-Jorgensen理论模型以及焓熵竞争模型等.文中较为详细地阐述了各种模型的内容、条件以及优缺点,并着重介绍了现在最为流行的Wolf热力学模型在剪切对二元和三元聚合物共混体系的理论研究中的具体应用.

参考文献

[1] Guo W;Higgins J .[J].S Polymer,1991,31:699.
[2] Utracki L A.Polymer Alloys and Blends[M].Haner, New York,1989
[3] Olabisi O;Roberson L M;Shaw M T.Polymer-Polymer Miscibility[M].Academic Press, London,1978
[4] Mazich K A;Carr S H .[J].Journal of Applied Physics,1983,54:5511.
[5] Katsaros J D;Malone M F;Winter H H .[J].Polymer Engineering and Science,1989,29:1434.
[6] Hindawi I A;Higgins J S;Weiss R A .[J].POLYMER,1992,33:2522.
[7] Rangel-Nafaile C;Motznor A;Wissbrun K .[J].Macromolecules,1984,17:1187.
[8] Wolf B A .[J].Macromolecules,1984,17:615.
[9] Horst R;Wolf B A .[J].Macromolecules,1992,25:5291.
[10] Onuki A .[J].Physical Review Letters,1989,62:2472.
[11] Ten B G;Szleifer I .[J].Macromolecules,1995,28:5434.
[12] Doi M;Onuki A .[J].Journal of De Physique Ⅱ,1992,2:1631.
[13] Fernandez ML.;Horst R.;Wolf BA.;Higgins JS. .COMPLEX MISCIBILITY BEHAVIOUR FOR POLYMER BLENDS IN FLOW[J].Polymer,1995(1):149-154.
[14] Horst R;Wolf B A .[J].Macromolecules,1993,26:5676.
[15] Horst R.;Wolf BA. .PHASE DIAGRAMS CALCULATED FOR SHEARED TERNARY POLYMER BLENDS[J].Polymer: The International Journal for the Science and Technology of Polymers,1997(18):4697-4703.
[16] Rabeony M;Siano D B;Peiffer D G et al.[J].Polymer,1994,35(05):1033.
[17] Helfand E;Fredrickson G H .[J].Physical Review Letters,1989,62:2468.
[18] Rector L P;Mazich K A;Carr S H .[J].Journal of Macromolecular Sciences:Physics,1988,B27(04):421.
[19] Lyngaae-Jorgensen J;Sondergaard K .[J].Polymer Engineering and Science,1987,27:351.
[20] Nakatani A I;Kim H;Takahashi Y et al.[J].Journal of Chemical Physics,1990,93:795.
[21] Kammer H W;Kummerloewe C;Kressler J et al.[J].POLYMER,1991,32(08):1488.
[22] Lyngaae-Jorgensen J;Sondergaard K .[J].Polymer Engineering and Science,1987,27:344.
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