Friday, August 22, 2008

3.4.4 HARDNESS (ASTM D 2240)

3.4.4 HARDNESS (ASTM D 2240):

SHORE – A:

The Shore – A Hardness test was performed as per the procedure explained in the chapter 2 and the results were tabulated as shown in table 3.15. From the results, regression analysis had been performed to get the regression equation, which is shown in the table 3.16. Then using the equation contour plots and response surfaces are generated which are shown in fig 3.21 and 3.22. The desired values of

Shore – A Hardness can be obtained at any combination within the optimized region as indicated in the contour plot. The value of X1 varies from 68 – 82 and X2 varies from 10 – 20 in the optimum region.

SHORE – D:

The Shore – A Hardness test was performed as per the procedure explained in the chapter 2 and the results were tabulated as shown in table 3.15. From the results, regression analysis had been performed to get the regression equation, which is shown in the table 3.17. Then using the equation contour plots and response surfaces are generated which are shown in fig 3.23 and 3.24. The desired values of

Shore – D Hardness can be obtained at any combination within the optimized region as indicated in the contour plot. The value of X1 varies from 55 - 67 and X2 17 - 25 varies from in the optimum region.

Table 3.15 Results of Shore – A and Shore – D Hardness tests for CaCO3 – HDPE system:

TRIAL

X1

X2

SHORE – A HARDNESS

SHORE – D

HARDNESS

1

60

5

76

54.3

2

60

25

79.0

56.0

3

80

5

81.0

58.3

4

80

25

78.3

56.3

5

56

15

78.3

59.0

6

84

15

80.3

58.0

7

70

1

78.0

57.3

8

70

29

80.6

57.3

9

70

15

81.0

57.6

10

70

15

81.0

57.6

11

70

15

81.0

57.6

Table 3.16 Estimated Regression Coefficients for Hardness- Shore A

Term

Coef

SE Coef

T

P

Constant

81.0095

0.4285

189.037

0.000

X1

0.9003

0.2638

3.413

0.019

X2

0.5119

0.2638

1.940

0.110

X1*X1

-1.0388

0.3166

-3.281

0.022

X2*X2

-1.0388

0.3166

-3.281

0.022

X1*X2

-1.4175

0.3712

-3.819

0.012

S = 0.7424 R-Sq = 90.3% R-Sq (adj) = 80.7%

The regression equation is

Y = 81.0095 +0.9003X1 +0.5119X2 -1.0388X12 -1.0388X22 -1.4175X1 X2.

Table 3.17 Estimated Regression Coefficients for Hardness- Shore D

Term

Coef

SE Coef

T

P

Constant

57.6223

0.8001

72.015

0.000

X1

0.3699

0.4925

0.751

0.486

X2

-0.0417

0.4925

-0.085

0.936

X1*X1

0.0210

0.5912

0.035

0.973

X2*X2

-0.5760

0.5912

-0.974

0.375

X1*X2

-0.9175

0.6930

-1.324

0.243

S = 1.386 R-Sq = 40.3% R-Sq (adj) = 0.0%

The regression equation is

Y = 57.6223 +0.3699X1 -0.0417X2 +0.0210X12 -0.576X22 -0.9175X1 X2.

Fig. 3.21 Contour Plot of Hardness – Shore A vs. X1, X2

Contour Plot of Hardness – Shore A vs. X1, X2

Fig. 3.22 Response surface of Hardness – Shore A vs. X1, X2

Response surface of Hardness – Shore A vs. X1, X2

Fig. 3.23 Contour plot of Hardness – Shore D vs. X1, X2


Contour plot of Hardness – Shore D vs. X1, X2

Fig. 3.24 Response surface of Hardness – Shore D vs. X1, X2

Response surface of Hardness – Shore D vs. X1, X2

OVERLAYING OF CONTOUR PLOTS:

The individual contour plots were generated for each of the property and then simultaneous optimization of properties were carried out by overlaying the individual plots to obtain the overlaid contour plots.

The desired values of all these properties can be obtained at any given combination within the optimized region indicated by the white coloured region in the fig.3.20. The values of both X1 and X2 vary over a wide range in the optimized region.

The desired values of all these properties can be obtained at any given combination within the optimized region indicated by the white coloured region in the fig.3.13. The value of X1 varies from 77 – 80 and X2 varies from 5 – 17 in the optimized region.

Fig. 3.20 Overlaid Contour plot of Tensile Properties

Overlaid Contour plot of Tensile Properties

Fig. 3.13 Overlaid contour Plot of Flexural Properties


Overlaid contour Plot of Flexural Properties

3.4.3 TENSILE PROPERTIES (ASTM D-638)

3.4.3 TENSILE PROPERTIES (ASTM D-638):

The tensile strength test was performed as per the procedure explained in the chapter 2 and the results were tabulated as shown in table 3.11. The properties that were evaluated as a part of tensile strength test are tensile strength at break load, percentage elongation at break load and Youngs modulus. From the results, regression analysis had been performed to get the regression equations, which are shown in the tables 3.12, 3.13, 3.14. Then using the equations contour plots and response surfaces were generated for each of them as shown in the figures 3.14 – 3.19.


Table 3.11 Results of Tensile Properties for CaCO3 – HDPE system

Trial no.

X1

X2

Youngs modulus

(kg/cm2 )

Tensile strength @ break load

(kg/cm2 )

Percentage elongation @ break load

1.

60

5

1214

104

80.2

2.

60

25

1157

119

66.5

3.

80

5

1337

159

90.5

4.

80

25

1205

176

174

5.

56

15

840

92.5

66.4

6.

84

15

1113

142

193

7.

70

1

1318

137

52

8.

70

29

1135

151

87

9.

70

15

1297

131

68.6

10.

70

15

1297

131

68.6

11.

70

15

1297

131

68.6


Table 3.12 Estimated Regression Coefficients for Tensile Strength @ break load

Term

Coef

SE Coef

T

P

Constant

130.882

5.054

25.895

0.000

X1

22.891

3.111

7.358

0.001

X2

6.515

3.111

2.094

0.090

X1*X1

-4.690

3.735

-1.256

0.265

X2*X2

8.958

3.735

2.399

0.062

X1*X2

0.500

4.378

0.114

0.914







S = 89.52 R-Sq = 80.4% R-Sq (adj) = 60.8%

The regression equation is

Y = 130.882+ 22.891X1 +6.515X2 -4.69X12 +8.958X22 +0.5X1 X2.


Table 3.13 Estimated Regression Coefficients for Tensile Strength Youngs Modulus

Term

Coef

SE Coef

T

P

Constant

1295.26

51.68

25.064

0.000

X1

69.85

31.81

2.196

0.080

X2

-56.21

31.81

-1.767

0.137

X1*X1

-129.30

38.18

-3.386

0.020

X2*X2

-1.74

38.18

-0.046

0.965

X1*X2

-18.75

44.76

-0.419

0.693

S = 89.52 R-Sq = 80.4% R-Sq (adj) = 60.8%

The regression equation is

Y = 1295.26+ 69.85X1 -56.21X2 -129.3X12 -1.74X22 -18.75X1 X2.

Table 3.14 Estimated Regression Coefficients for Percentage Elongation

Term

Coef

SE Coef

T

P

Constant

68.566

6.073

11.290

0

X1

37.253

3.738

9.965

0

X2

15

3.738

4.012

0.01

X1*X1

31.846

4.488

7.096

0.001

X2*X2

1.131

4.488

0.252

0.811

X1*X2

24.3

5.260

4.619

0.006

S = 10.52 R-Sq = 97.41% R-Sq (adj) = 94.9%

The regression equation is

Y = 68.566+ 37.253X1 +15X2 +31.846X12 +1.131X22 +24.3X1 X2.


Fig. 3.14 Contour Plot of tensile strength at break load vs. X2, X1

Contour Plot of tensile strength at break load vs. X2, X1

Fig. 3.15 Response surface of tensile strength at break load vs. X2, X1


Response surface of tensile strength at break load vs. X2, X1

Fig. 3.16 Plot of Youngs Modulus vs. X1


Plot of Youngs Modulus vs. X1

Fig. 3.17 Response surface of Youngs Modulus vs. X2, X1

Response surface of Youngs Modulus vs. X2, X1

Fig. 3.18 Contour plot of Percentage Elongation vs. X2, X1

Fig. 3.18 Contour plot of Percentage Elongation vs. X2, X1

Fig. 3.19 Response surface of Percentage Elongation vs. X2, X1



Response surface of Percentage Elongation vs. X2, X1