Hi, can you help me provide the step-by-step working solution for part (b) of the above question?
A titanium-nickel alloy is a superalloy. It is mostly used for making jet turbine aircraft engines. Jet turbines work from high cyclic dynamic, thermal loads are acting on the jet engine body. Therefore, cracking is occurs in their parts and it is a very sober problem So, that we make an experimental test for four factors on cracks.
The four fours are pouring temperature (A), titanium (B), heat treatment (C), amount of grain refiner used (D). The best optimum technique can be a 24 Experiment design technique, which is developed by Dr. Taguchi.
The data are shown below in the design table and total of the replica I and II and the effect of factors
A | B | C | D | Replicate I | Replicate II | Total |
-1 | -1 | -1 | -1 | 7.037 | 6.376 | 13.413 |
1 | -1 | -1 | -1 | 14.7.7 | 15.219 | 15.219 |
-1 | 1 | -1 | -1 | 11.635 | 12.089 | 23.724 |
1 | 1 | -1 | -1 | 17.273 | 17.815 | 35.088 |
-1 | -1 | 1 | -1 | 10.403 | 10.151 | 20.554 |
1 | -1 | 1 | -1 | 4.368 | 4.098 | 8.466 |
-1 | 1 | 1 | -1 | 9.36 | 9.253 | 18.613 |
1 | 1 | 1 | -1 | 13.44 | 12.923 | 26.363 |
-1 | -1 | -1 | 1 | 8.561 | 8.951 | 17.512 |
1 | -1 | -1 | 1 | 16.867 | 17.052 | 33.919 |
-1 | 1 | -1 | 1 | 13.876 | 13.658 | 27.534 |
1 | 1 | -1 | 1 | 19.824 | 19.639 | 39.463 |
-1 | -1 | 1 | 1 | 11.846 | 12.337 | 24.183 |
1 | -1 | 1 | 1 | 6.125 | 5.904 | 12.029 |
-1 | 1 | 1 | 1 | 11.19 | 10.935 | 22.125 |
1 | 1 | 1 | 1 | 15.653 | 15.053 | 30.706 |
The Factors effect plot
Fitted Line plot for Factor A
Fitted Line plot for Factor B
Fitted Line plot for Factor C
Fitted Line plot for Factor D
Minitab Output
Fitted Line: D versus Replicate I & II
Regression Analysis: Replicate I & II versus A, B, C, D
The regression equation is
Replicate I & II = 23.1 + 2.10 A + 4.90 B - 2.68 C + 2.88 D
Predictor Coef SE Coef T P
Constant 23.057 1.632 14.13 0.000
A 2.100 1.632 1.29 0.225
B 4.895 1.632 3.00 0.012
C -2.677 1.632 -1.64 0.129
D 2.877 1.632 1.76 0.106
S = 6.52716 R-Sq = 59.9% R-Sq(adj) = 45.4%
Analysis of Variance
Source DF SS MS F P
Regression 4 701.02 175.26 4.11 0.028
Residual Error 11 468.64 42.60
Total 15 1169.66
Source DF Seq SS
A 1 70.54
B 1 383.39
C 1 114.67
D 1 132.43
Hi, can you help me provide the step-by-step working solution for part (b) of the above...
use the half normal plot to determine factors that are significant. 1. A nickel-titanium alloy is used to make components for jet turbine aircraft engines. Cracking is a potentally serious problem in the final part, as it can lead to non-recoverable failure. A test is run at the parts producer to determine the effects of four factors on cracks. The four factors are pouring temperature (A), itanium content (B), heat treatment method (C), and the amount of grain refiner used...
Please show calculations using MINITAB PROBLEM 1 A nickel-titanium alloy is. used to make components for jet turbine aircraft engines. Cracking is a potentially serious problem in the final part because it can lead to non-recoverable failure. A test is run at the parts produced to determine the effect of four factors on cracks. The four factors are A pouring temperature Btitanium content C = heat treatment method D amount of grain refiner used Two replicates of a 2 design...