Solution Found!
Cooling method for gas turbines. Refer to the Journalof
Chapter 12, Problem 130E(choose chapter or problem)
Cooling method for gas turbines. Refer to the Journal Of Engineering for Gas Turbines and Power (Jan. 2005)study of a high-pressure inlet fogging method for a gas turbine engine, Exercise 12.103 (p. 729). Now consider the interaction model for heat rate (y) of a gas turbine as a function of cycle speed (\(x_1\)) and cycle pressure ratio (\(x_2\)), \(E(y)=\beta_0+\beta_1x_1+\beta_2x_2+\beta_3x_1x_2\). Use the data saved in the file to conduct a complete residual analysis for the model. Do you recommend making model modifications?
Questions & Answers
QUESTION:
Cooling method for gas turbines. Refer to the Journal Of Engineering for Gas Turbines and Power (Jan. 2005)study of a high-pressure inlet fogging method for a gas turbine engine, Exercise 12.103 (p. 729). Now consider the interaction model for heat rate (y) of a gas turbine as a function of cycle speed (\(x_1\)) and cycle pressure ratio (\(x_2\)), \(E(y)=\beta_0+\beta_1x_1+\beta_2x_2+\beta_3x_1x_2\). Use the data saved in the file to conduct a complete residual analysis for the model. Do you recommend making model modifications?
ANSWER:Step 1 of 8
Let y be the heat rate of a gas turbine, is the cycle speed and is the cycle pressure
ratio.
Here we have to obtain the estimated model, and
conduct a complete residual analysis for the model.
Using MINITAB, we fit the above model and conduct the residual analysis for the
fitted model in the following steps.
Step1: Import the data into the columns of the worksheet and find the product value of
and in another column (named ).
Step2: Select Regression... ?om the Regression tab of Stat ribbon.
Step3: Specify the column y in the Response box and the columns , and , as
Predictors.
Step4: Check Histogram of residuals, Residuals versus fits, and Residual versus
order in Residual plots and specify the columns , and in Residuals
versus the variables in the Graphs... tab.
Step5: Click Ok.