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: 408 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 02 Nov 2017 My Price 7.00

Gas Turbines and Power

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 (x1), inlet temperature (x2), exhaust tem- perature (x3), cycle pressure ratio (x4), and air flow rate (x5) to data saved in the GASTURBINE file.

 

(a)    Researchers hypothesize that the linear relationship between heat rate (y) and tem- perature (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 GASTUR- BINE 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

Answers

Maurice Tutor
(5)
Status NEW Posted 02 Nov 2017 06:11 PM My Price 7.00

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