Cooling method for gas turbines

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Cooling method for gas turbines

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, inlet temperature, exhaust temperature, cycle pressure ratio, and air flow rate, to data saved in the GASTURBINE file.

  • Budget: $10 Ready
  • Posted by: Kumyiah108
  • Subjects: Math Environmental Law
  • Attachments: Statistics II Week 3 Homework.docx (27 KB)

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