Solution Found!
Cooling method for gas turbines. Refer to the Journal of
Chapter 7, Problem 94E(choose chapter or problem)
Cooling method for gas turbines. Refer to the Journal of Engineering for Gas Turbines and Power (Jan. 2005) study of the performance of augmented gas turbine engines, Exercise 7.40 (p. 378). Recall that performance for each in a sample of 67 gas turbines was measured by heat rate (kilojoules per kilowatt per hour). The data are saved in the accompanying file. Suppose that standard gas turbines have heat rates with a standard deviation of 1,500 kJ/kWh. Is there sufficient evidence to indicate that the heat rates of the augmented gas turbine engine are more variable than the heat rates of the standard gas turbine engine? Test using \(\alpha\) = .05.
Questions & Answers
QUESTION:
Cooling method for gas turbines. Refer to the Journal of Engineering for Gas Turbines and Power (Jan. 2005) study of the performance of augmented gas turbine engines, Exercise 7.40 (p. 378). Recall that performance for each in a sample of 67 gas turbines was measured by heat rate (kilojoules per kilowatt per hour). The data are saved in the accompanying file. Suppose that standard gas turbines have heat rates with a standard deviation of 1,500 kJ/kWh. Is there sufficient evidence to indicate that the heat rates of the augmented gas turbine engine are more variable than the heat rates of the standard gas turbine engine? Test using \(\alpha\) = .05.
ANSWER:Step 1 of 2
The experiment under consideration is the study of the performance of the augmented gas turbine engines.
The data regarding the performance of 67 gas turbines are given.
14622 |
13196 |
11948 |
11289 |
11964 |
10526 |
10387 |
10592 |
10460 |
10086 |
14628 |
13396 |
11726 |
11252 |
12449 |
11030 |
10787 |
10603 |
10144 |
11674 |
11510 |
10946 |
10508 |
10604 |
10270 |
10529 |
10360 |
14796 |
12913 |
12270 |
11842 |
10656 |
11360 |
11136 |
10814 |
13523 |
11289 |
11183 |
10951 |
9722 |
10481 |
9812 |
9669 |
9643 |
9115 |
9115 |
11588 |
10888 |
9738 |
9095 |
9421 |
9105 |
10233 |
10186 |
9918 |
9209 |
9532 |
9933 |
9152 |
9295 |
16243 |
14628 |
12766 |
8714 |
9469 |
11948 |
12414 |
Also, it is given that the standard deviation of heat rates for the standard gas turbines is 1,500kj/kWh.
Using this data we have to test is there any evidence to say that the heat rates of the augmented gas turbine engines are more variable than the heat rates of the standard gas turbine engines at =0.05.