Maurice Tutor

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About Maurice Tutor

Levels Tought:
Elementary,Middle School,High School,College,University,PHD

Expertise:
Algebra,Applied Sciences See all
Algebra,Applied Sciences,Biology,Calculus,Chemistry,Economics,English,Essay writing,Geography,Geology,Health & Medical,Physics,Science Hide all
Teaching Since: May 2017
Last Sign in: 407 Weeks Ago, 5 Days Ago
Questions Answered: 66690
Tutorials Posted: 66688

Education

  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

Experience

  • Professor
    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 29 Sep 2017 My Price 8.00

Engineering for Gas Turbines

4.24              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

 

 

 

MINITAB Output for Exercise 4.24

 

 

speed (x1), inlet temperature (x2), exhaust tem- perature (x3), cycle pressure ratio (x4), and air flow rate (x5) to data saved in the GASTUR- BINE file. A MINITAB printout with both a 95% confidence interval for E(y) and prediction interval for y for selected values of the x’s is shown below.

 

 

 

 

 

 

(a)    Interpret the 95% prediction interval for y in the words of the problem.

 

(b)    Interpret the 95% confidence interval for

 

E(y) in the words of the problem.

 

(c)    Will the confidence interval for E(y) always be narrower than the prediction interval for y? Explain.

 

 

 


Answers

Maurice Tutor
(5)
Status NEW Posted 29 Sep 2017 09:09 PM My Price 8.00

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