6-46. The data shown in Table 6-15 represent the thrust of a jet-turbine engine (y) and six candidate regressors: x₁ = pri- mary speed of rotation, x₂ = secondary speed of rotation, x3 fuel flow rate, x₁ pressure, x, = exhaust temperature, and x = ambient temperature at time of test. = = X6 (a) Fit a multiple linear regression model using x, = fuel flow rate, X4 = pressure, and x = exhaust temperature as the regressors. (b) Test for significance of regression using a = 0.01. Find

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using r- studio please cod the following parts a-h

=
pri-
6-46. The data shown in Table 6-15 represent the thrust of a
jet-turbine engine (y) and six candidate regressors: x₁
mary speed of rotation, x₂ = secondary speed of rotation, x3
fuel flow rate, x = pressure, x, = exhaust temperature, and
x6 = ambient temperature at time of test.
(a) Fit a multiple linear regression model using x, = fuel flow
rate, x4 pressure, and x5 exhaust temperature as the
=
=
regressors.
(b) Test for significance of regression using a = 0.01. Find
the P-value for this test. What are your conclusions?
(c) Find the t-test statistic for each regressor. Using a = 0.01,
explain carefully the conclusion you can draw from these
statistics.
(d) Find R2 and the adjusted statistic for this model. Comment
on the meaning of each value and its usefulness in assess-
ing the model.
(e) Construct a normal probability plot of the residuals and
interpret this graph.
(f) Plot the residuals versus y. Are there any indications of
inequality of variance or nonlinearity?
(g) Plot the residuals versus x3. Is there any indication of non-
linearity?
(h) Predict the thrust for an engine for which x3
-
X4 = 170, and x = 1589.
= 20000,
Transcribed Image Text:= pri- 6-46. The data shown in Table 6-15 represent the thrust of a jet-turbine engine (y) and six candidate regressors: x₁ mary speed of rotation, x₂ = secondary speed of rotation, x3 fuel flow rate, x = pressure, x, = exhaust temperature, and x6 = ambient temperature at time of test. (a) Fit a multiple linear regression model using x, = fuel flow rate, x4 pressure, and x5 exhaust temperature as the = = regressors. (b) Test for significance of regression using a = 0.01. Find the P-value for this test. What are your conclusions? (c) Find the t-test statistic for each regressor. Using a = 0.01, explain carefully the conclusion you can draw from these statistics. (d) Find R2 and the adjusted statistic for this model. Comment on the meaning of each value and its usefulness in assess- ing the model. (e) Construct a normal probability plot of the residuals and interpret this graph. (f) Plot the residuals versus y. Are there any indications of inequality of variance or nonlinearity? (g) Plot the residuals versus x3. Is there any indication of non- linearity? (h) Predict the thrust for an engine for which x3 - X4 = 170, and x = 1589. = 20000,
Y
X4 X5 X6
4540 2140 20640 30250 205 1732 99
X1 X2
X3
نت
4315 2016 20280 30010 195 1697 100
4095 1905 19860
29780 184 1662 97
3650 1675 18980
29330 164 1598 97
3200 1474 18100 28960 144 1541 97
4833 2239 20740 30083 215 1709 87
4617 2120 20305 29831 206 1669 87
4340 1990 19961 29604 195 1640 87
3820 1702 18916 29088 171 1572 85
3368 1487 18012 28675 149 1522 85
4445 2107 20520 30120 195 1740 101
4188 1973 20130 29920 190 1711 100
3981 1864 19780 29720 180 1682 100
3622 1674 19020 29370 161 1630 100
3125 1440 18030
1572 101
4560 2165 20680 30160
208 1704 98
4340 2048 20340 29960 199
1679 96
4115 1916 19860
29710 187 1642 94
3630 1658 18950
29250 164 1576 94
3210 1489 18700
28890 145 1528 94
4330 2062 20500
30190 193 1748 101
4119 1929 20050 29960 183 1713 100
3891 1815 19680 29770 173 1684 100
3467 1595 18890 29360 153 1624 99
3045 1400 17870 28960 134 1569 100
4411 2047 20540 30160 193 1746 99
4203 1935 20160 29940 184 1714 99
3968 1807 19750 29760 173 1679 99
28940 139
3531 1591 18890 29350 153 1621 99
3074 1388 17870 28910 133 1561 99
4350 2071 20460 30180 198 1729 102
4128 1944 20010 29940 186 1692 101
3940 1830 19640 29750 178 1667 101
3480 1612 18710 29360 156 1609 101
3064 1410 17780 28900 136 1552 101
4402 2066 20520 30170 197 1758 100
4180 1954 20150 29950 188 1729 99
3973 1835 19750 29740 178 1690 99
3530 1616 18850 29320 156 1616 99
3080 1407 17910 28910 137 1569 100
Transcribed Image Text:Y X4 X5 X6 4540 2140 20640 30250 205 1732 99 X1 X2 X3 نت 4315 2016 20280 30010 195 1697 100 4095 1905 19860 29780 184 1662 97 3650 1675 18980 29330 164 1598 97 3200 1474 18100 28960 144 1541 97 4833 2239 20740 30083 215 1709 87 4617 2120 20305 29831 206 1669 87 4340 1990 19961 29604 195 1640 87 3820 1702 18916 29088 171 1572 85 3368 1487 18012 28675 149 1522 85 4445 2107 20520 30120 195 1740 101 4188 1973 20130 29920 190 1711 100 3981 1864 19780 29720 180 1682 100 3622 1674 19020 29370 161 1630 100 3125 1440 18030 1572 101 4560 2165 20680 30160 208 1704 98 4340 2048 20340 29960 199 1679 96 4115 1916 19860 29710 187 1642 94 3630 1658 18950 29250 164 1576 94 3210 1489 18700 28890 145 1528 94 4330 2062 20500 30190 193 1748 101 4119 1929 20050 29960 183 1713 100 3891 1815 19680 29770 173 1684 100 3467 1595 18890 29360 153 1624 99 3045 1400 17870 28960 134 1569 100 4411 2047 20540 30160 193 1746 99 4203 1935 20160 29940 184 1714 99 3968 1807 19750 29760 173 1679 99 28940 139 3531 1591 18890 29350 153 1621 99 3074 1388 17870 28910 133 1561 99 4350 2071 20460 30180 198 1729 102 4128 1944 20010 29940 186 1692 101 3940 1830 19640 29750 178 1667 101 3480 1612 18710 29360 156 1609 101 3064 1410 17780 28900 136 1552 101 4402 2066 20520 30170 197 1758 100 4180 1954 20150 29950 188 1729 99 3973 1835 19750 29740 178 1690 99 3530 1616 18850 29320 156 1616 99 3080 1407 17910 28910 137 1569 100
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