A study of a high-pressure inlet fogging method for a gas turbine engine analyzed a complete second-order model for y , heat rate (kilojoules per kilowatt per hour) of a gas turbine as a function of...


A study of a high-pressure inlet fogging method for a gas turbine<br>engine analyzed a complete second-order model for y , heat rate<br>(kilojoules per kilowatt per hour) of a gas turbine as a function of two<br>quantitative variables<br>• x1 , cycle speed (revolutions per minute)<br>• x2 , cycle pressure ratio<br>and a qualitative predictor, engine type, at three levels (traditional,<br>advanced, and aeroderivative).<br>We define two dummy variables<br>S 1<br>{o if<br>if advanced<br>if aeroderivative<br>and x4<br>X3 =<br>not<br>0 if not<br>Write a complete second-order model for heat rate (y ) as a function of<br>cycle speed, cycle pressure ratio, and engine type.<br>

Extracted text: A study of a high-pressure inlet fogging method for a gas turbine engine analyzed a complete second-order model for y , heat rate (kilojoules per kilowatt per hour) of a gas turbine as a function of two quantitative variables • x1 , cycle speed (revolutions per minute) • x2 , cycle pressure ratio and a qualitative predictor, engine type, at three levels (traditional, advanced, and aeroderivative). We define two dummy variables S 1 {o if if advanced if aeroderivative and x4 X3 = not 0 if not Write a complete second-order model for heat rate (y ) as a function of cycle speed, cycle pressure ratio, and engine type.

Jun 04, 2022
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