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).

Algebra & Trigonometry with Analytic Geometry
13th Edition
ISBN:9781133382119
Author:Swokowski
Publisher:Swokowski
Chapter7: Analytic Trigonometry
Section7.6: The Inverse Trigonometric Functions
Problem 91E
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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
0 if not
{
if advanced
1
if aeroderivative
X3 =
and
X4
if not
If the engine type is traditional, then x3 =
and x4
When you plug in these two values in the
complete second-order model equation, you will get the model
equation for traditional engine type.
Transcribed Image 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 0 if not { if advanced 1 if aeroderivative X3 = and X4 if not If the engine type is traditional, then x3 = and x4 When you plug in these two values in the complete second-order model equation, you will get the model equation for traditional engine type.
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