4.32 Cooling method for gas turbines. Refer to the Journal of Engineering for Gas Turbines and Power (January 2005) study of a high-pressure inlet fogging method for a gas turbine engine, Exercise 4.13 (p.188). Recall that you fit a first-order model for heat rate (y) as a function of speed(π₯1 ), inlet temperature(π₯2 ), exhaust temperature(π₯3 ), cycle pressure ratio(π₯4 ), and air flow rate(π₯5 ), to data saved in the GASTURBINE file. a. Researchers hypothesize that the linear relationship between heat rate (y) and temperature (both inlet and exhaust) depends on air flow rate. Write a model for heat rate that incorporates the researchers’ theories. b. Use statistical software to fit the interaction model, part a, to the data in the GASTURBINE file. Give the least squares prediction equation. c. Conduct a test (at α=.05) to determine whether inlet temperature and air flow rate interact to effect heat rate. d. Conduct a test (at α=.05) to determine whether exhaust temperature and air flow rate interact to effect heat rate. e. Practically interpret the results of the tests, parts c and d. 4.36 Cars with catalytic converters. A quadratic model was applied to motor vehicle toxic emissions data collected over 15 recent ears in Mexico City (Environment Science and Engineering, September 1, 2000). The following equation was used to predict the percentage (y) of motor vehicles without catalytic converters in the Mexico City fleet for a given year (π₯): π¦ = 325,790 − 321.67π₯ + 0.794π₯ 2 . a. Explain why the value π½0 = 325,790 has no practical interpretation. b. Explain why the value π½1 = 321.67 should not be interpreted as a slope. c. Examine the value of π½2 to determine the nature of the curvature (upward or downward) in the sample data. d. The researchers used the model to estimate “that just after the year 2021 the fleet of cars with catalytic converters will completely disappear.” Comment on the danger of using the model to predict y in the year 2021. 4.40 Failure times of silicon wafer microchips. Researchers at National Semiconductor experimented with tin-lead solder bumps used to manufacture silicon wafer integrated circuit chips (International Wafer Level Packaging Conference, November 3-4, 2005). The failure times of the microchips (in hours) were determined at different solder temperatures (degrees Centigrade). The data for one experiment are given in the next table (p.208). The researchers want to predict failure time (y) based on solder temperature (x). a) Construct a scatterplot for the data. What type of relationship, linear or curvilinear, appears to exist between failuretime and solder temperature? Scatterplot of TEMP vs FAILTIME 170 160 TEMP 150 140 130 120 110 0 2000 4000 6000 8000 10000 FAILTIME b) Fit the model (π¦) = π½0 + π½1 π₯ + π½2 π₯ 2 , to the data. Give the least squares prediction equation. S = 5.26788 R-Sq = 84.3% R-Sq(adj) = 83.5% Analysis of Variance Source Regression Error Total DF 1 20 21 SS 2978.26 555.01 3533.27 MS 2978.26 27.75 F 107.32 P 0.000 Fitted Line Plot TEMP = 158.7 - 0.004400 FAILTIME 170 S R-Sq R-Sq(adj) 160 5.26788 84.3% 83.5% TEMP 150 140 130 120 110 0 2000 4000 6000 8000 10000 FAILTIME Fitted Line: TEMP versus FAILTIME c) Conduct a test to determine if there is upward curvature in the relationship between failuretime and solder temperature. (Use α=.05) The prediction is less robust to departures from normality. The distinction between variability and uncertainty is useful in understanding the distinction between confidence intervals for the conditional mean and prediction intervals: The confidence interval for the conditional mean measures our degree of uncertainty in our estimate of the conditional mean; but the prediction interval must also take into account the variability in the conditional distribution. 4.64 Cooling method for gas turbines. Refer to the Journal of Engineering for Gas Turbines and Power (January 2005) study of a high-pressure inlet fogging method for a gas turbine engine, Exercise 4.13 (p.188). Consider a model for heat rate (kilojoules per kilowatt per hour) of a gas turbine as a function of cycle speed (revolutions per minute) and cycle pressure ratio. The data are saved in the GASTURBINE file. a) Write a complete second-order model for heat rate (y). b) Give the null and alternative hypothesis for determining whether the curvature terms in the complete second-order model are statistically useful for predicting heat rate (y). c) For the test in part b, identify the “complete” and “reduced” model. d) Portions of the MINITAB printouts for the two models are shown below. Find the values of πππΈπ , πππΈπΆ , πππ πππΈπΆ on the printouts. e) Compute the value of the test statistics for the test of part b. f) Find the rejection region for the test of part b using α=.10. g) Stat the conclusion of the test in the words of the problem.