need step by step for MINITAB please
Problem 1. Consider the GASTURBINE data set and corresponding output from Minitab. Use the complete data set in your analysis. The first 10 observations are given for illustrative purposes. Complete parts a) through g) below.
ENGINE |
SHAFTS |
RPM |
CPRATIO |
INLET-TEMP |
EXH-TEMP |
AIRFLOW |
POWER |
HEATRATE |
Traditional |
1 |
27245 |
9.2 |
1134 |
602 |
7 |
1630 |
14622 |
Traditional |
1 |
14000 |
12.2 |
950 |
446 |
15 |
2726 |
13196 |
Traditional |
1 |
17384 |
14.8 |
1149 |
537 |
20 |
5247 |
11948 |
Traditional |
1 |
11085 |
11.8 |
1024 |
478 |
27 |
6726 |
11289 |
Traditional |
1 |
14045 |
13.2 |
1149 |
553 |
29 |
7726 |
11964 |
Traditional |
1 |
6211 |
15.7 |
1172 |
517 |
176 |
52600 |
10526 |
Traditional |
1 |
6210 |
17.4 |
1177 |
510 |
193 |
57500 |
10387 |
Traditional |
1 |
3600 |
13.5 |
1146 |
503 |
315 |
89600 |
10592 |
Traditional |
1 |
3000 |
15.1 |
1146 |
524 |
375 |
113700 |
10460 |
Traditional |
1 |
3000 |
15 |
1171 |
525 |
514 |
164300 |
10086 |
Regression Analysis: HEATRATE versus RPM, CPRATIO, …
The regression equation is
HEATRATE = 14314 + 0.0806 RPM - 6.8 CPRATIO - 9.51 INLET-TEMP + 14.2 EXH-TEMP
- 2.55 AIRFLOW + 0.00426 POWER
Predictor Coef SE Coef T P
Constant 14314 1112 12.87 0.000
RPM 0.08058 0.01611 5.00 0.000
CPRATIO -6.78 30.38 -0.22 0.824
INLET-TEMP -9.507 1.529 -6.22 0.000
EXH-TEMP 14.155 3.469 4.08 0.000
AIRFLOW -2.553 1.746 -1.46 0.149
POWER 0.004257 0.004217 1.01 0.317
S = 458.757 R-Sq = 92.5% R-Sq(adj) = 91.7%
Analysis of Variance
Source DF SS MS F P
Regression 6 155269735 25878289 122.96 0.000
Residual Error 60 12627473 210458
Total 66 167897208
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