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Shrinkage predicting

This analysis reveals that measurement of shrinkage or linear coefficients of thermal expansion (CTE s) in just flow and width directions, as is done for conventional polymers, is not sufficient for liquid crystal polymers (LCP s) and can lead to erroneous shrinkage predictions. This is a consequence of inherent LCP anisotropy, resulting in a relatively large linear CTE and shrinkage in the thickness direction of associated molded LCP parts. Linear and volumetric CTE data for neat and filled LCP molded parts of different geometries are presented. [Pg.381]

Table II giveB a comparison of actual XYDAR molded part shrinkages vs shrinkages predicted upon cooling from melt and mold temperatures for 45% glass fiber (G-445) and 50% mineral/glass fiber (MG-350) compositions. These predicted values were estimated using equations (5) S (6) in the theory Bection. Table II giveB a comparison of actual XYDAR molded part shrinkages vs shrinkages predicted upon cooling from melt and mold temperatures for 45% glass fiber (G-445) and 50% mineral/glass fiber (MG-350) compositions. These predicted values were estimated using equations (5) S (6) in the theory Bection.
Snyder, J. A., Mold Design Software Makes Part Shrinkage Predictable, MP, pp. 10-11, Jan. 1989. [Pg.372]

C PACK (Advanced CAE Technology, Inc., Ithaca, NY). Calculates volumetric shrinkage of analyzed elements in terms of density differences between in-mold and stabilized conditions. Linear shrinkage prediction not yet available. [Pg.934]

Next, a one hidden layer model of neural network reveals that the network 5-11-1 provides the most accuracy of o-ring shrinkage prediction as shown in Table... [Pg.1467]

As a first approximation, a superposition method has been used that can provide a guide to predicting mold shrinkage (Fig. 3-27). However, problems arise in measuring the influencing variables, because they... [Pg.171]

Computer-aided flow-simulation programs are also available for dies. All the programs can successfully predict a certain amount of shrinkage under specific conditions that can be applied to experience. The actual shrinkage is finally determined after molding or extruding the products. When not in spec process control changes can meet the requirements unless some drastic error had been included in the analysis. [Pg.443]

In most instances, external-beam radiation therapy used in conjunction with breast-conserving procedures involves 4 to 6 weeks of radiation therapy directed to the breast tissue to eradicate residual disease. Complications associated with radiation therapy to the breast are minor and include reddening and erythema of the breast tissue and subsequent shrinkage of total breast mass beyond that predicted on the basis of breast tissue removal. Some clinical situations also require postmastectomy radiation therapy as well (see section on locally advanced breast cancer). [Pg.1309]

The experimental determination of RBA, however, is difficult but some attempts have been made and these include direct observation, measurements of electrical conductivity, shrinkage energy, gas adsorption and light scattering. The linear elastic response of paper has been explained in terms of various micromechanical models which take into account both fibre and network properties, including RBA. An example of one which predicts the sheet modulus, Es is given below ... [Pg.65]

The sigma lone pair nonbonded interaction in F2C=CH2 can be treated in a similar fashion. The appropriate interaction diagram is shown in Fig. 15 and our conclusions are identical to the ones reached in the case of F2CH2, i.e. nonbonded attraction between the fluorine 2px lone pairs favors angle shrinkage in CF2=CH2. The results of calculations shown above are, once again, in agreement with these predictions. [Pg.54]

The optimization of the moulding parameters can be difficult because of the delicate balance between the blowing agent decomposition and the part shaping. Part warpage and shrinkage are sometimes difficult to predict. [Pg.741]

Fig. 7.24. Predicted fracture toughness of carbon and glass fiber-polymer matrix composites (CFRP and GFRP) with varying matrix shrinkage stress, n. After Piggott (1981). Fig. 7.24. Predicted fracture toughness of carbon and glass fiber-polymer matrix composites (CFRP and GFRP) with varying matrix shrinkage stress, n. After Piggott (1981).

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