Refer to the Journal of Engineering for Gas Turbines and Power (Jan. 2005) study of three types of gas turbines augmented with high pressure inlet fogging, Exercise 8.39. Heat rate data (kilojoules per kilowatt per hour) for advanced and aero derivative gas turbines are shown in the table. Use the bootstrap procedure to test (at α = .05) for a difference between the mean heat rates of advanced augmented gas turbines and aero derivative augmented gas turbines. Compare the bootstrap ASL to the p-value obtained from the test in Exercise 8.39b.

Data from Exercise 8.39

Refer to the Journal of Engineering for Gas Turbines and Power (Jan. 2005) study of gas turbines augmented with high-pressure inlet fogging, Exercise 8.29. The researchers classified gas turbines into three categories: traditional, advanced, and aero derivative. Summary statistics on heat rate (kilojoules per kilowatt per hour) for each of the three types of gas turbines in the sample are shown in the MINITAB printout.

Transcribed Image Text:

GASTURBINE Advanced: 9722 10481 9812 9669 9643 9115 9115 11588 10888 9738 9295 9421 9105 10233 10186 9918 9209 9532 9933 9152 9295 Aeroderivative: 16243 14628 12766 8714 9469 11948 12414