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Evaluation of the tensile stress-strain properties in the thickness ...

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placements along <strong>the</strong> <strong>thickness</strong> direction <strong>in</strong> three<br />

different po<strong>in</strong>ts outside <strong>the</strong> test piece. The displacements<br />

<strong>of</strong> all po<strong>in</strong>ts belong<strong>in</strong>g to <strong>the</strong> same plane are given by<br />

ax + by + cz + d =0. [A1.1]<br />

The unknowns <strong>in</strong> <strong>the</strong> Eq (1) are <strong>the</strong> three cos<strong>in</strong>e directors<br />

a /d b /d c /d. The unknowns can be evaluated by substitut<strong>in</strong>g<br />

<strong>of</strong> <strong>the</strong> coord<strong>in</strong>ates three sensors <strong>in</strong>to Eq (1), be<strong>in</strong>g <strong>the</strong><br />

position <strong>in</strong> <strong>the</strong> x-y plane <strong>the</strong> x i,y i coord<strong>in</strong>ates and z i <strong>the</strong><br />

displacement along <strong>the</strong> <strong>thickness</strong> direction:<br />

⎡−1⎤<br />

⎡x<br />

y z ⎤⎡a<br />

d⎤<br />

1 1 1<br />

⎢ ⎥ ⎢ ⎥⎢<br />

⎥<br />

⎢−1⎥<br />

= ⎢x<br />

y z<br />

2 2 2⎥⎢bd⎥<br />

⎢<br />

⎣−1⎥<br />

⎢<br />

⎦ ⎣x<br />

y z ⎥⎢<br />

⎥<br />

3 3 3⎦⎣cd⎦<br />

The deformation <strong>of</strong> <strong>the</strong> centre <strong>of</strong> <strong>the</strong> test piece z center was<br />

determ<strong>in</strong>ed by substitut<strong>in</strong>g <strong>the</strong> coord<strong>in</strong>ate <strong>of</strong> <strong>the</strong> centre<br />

x center=0 and y center =0 <strong>in</strong>to (A1.1)<br />

z<br />

center<br />

−c<br />

=<br />

d<br />

Appendix II<br />

56 Nordic Pulp and Paper Research Journal Vol 22 no. 1/2007<br />

[A1.2]<br />

[A1.3]<br />

Table AII:1. Experimental results <strong>of</strong> Z-directional strength, elastic modulus and <strong>stra<strong>in</strong></strong> at break<br />

for <strong>the</strong> tested pulps.<br />

Grammage Z-directional 95% Z-directional 95% Elastic 95% Stra<strong>in</strong> 95%<br />

kg/m 2<br />

<strong>tensile</strong> CI <strong>tensile</strong> strength CI Modulus CI at break CI<br />

strength kPa (tape) kPa MPa %<br />

TMP1<br />

100 197 14 188 12 7.1 2.8 12.5 2.1<br />

120 215 33 204 17 7.9 3.7 10.5 0.8<br />

180 233 11 225 5 9.5 2.1 9.3 1.1<br />

240 220 10 215 9 7.7 2.2 8.7 0.7<br />

300 220 10 232 11 9.4 1.0 8.3 1.0<br />

TMP2<br />

80 335 42 323 16 13.3 3.7 12.6 0.8<br />

100 353 16 312 17 16.7 2.5 10.2 0.5<br />

120 384 17 328 46 19.6 3.7 9.0 0.8<br />

180 400 15 344 18 19.6 2.8 8.2 0.4<br />

240 375 15 352 27 16.01 2.7 8.4 0.4<br />

300 332 12 354 7 13.6 2.1 8.4 0.7<br />

Chem1<br />

80 777 99 442 3.2 62 26.7 2.7 1.2<br />

100 699 36 424 17.7 67 15.7 2.4 0.4<br />

120 655 7 409 8.9 91 14.6 2.0 0.6<br />

180 611 8 505 14 73 18.9 2.2 0.2<br />

240 550 11 484 5 73 9.5 1.7 0.1<br />

300 529 8 488 10 71 11.3 1.4 0.2<br />

Chem2<br />

80 1946 38 717 7.3 188.6 75.9 2.8 1.2<br />

100 1936 29 716 6.2 169.0 26.6 3.4 0.4<br />

120 1916 39 719 7.6 217.3 62.5 2.6 0.6<br />

180 1833 53 688 19 203.4 25.4 2.0 0.2<br />

240 1781 24 683 14 205.5 31.8 1.9 0.1<br />

300 1693 37 683 11 206.0 16.9 1.8 0.2<br />

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Determ<strong>in</strong>ation <strong>of</strong> fiber-fiber bond <strong>properties</strong>, New York.<br />

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Manuscript received August 30, 2006<br />

Accepted November 10, 2006

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