Cooling method for gas turbines. During periods of high electricity demand, especially during the hot summer months, the power output from a gas turbine engine can drop dramatically. One way to counter this drop in power is by cooling the inlet air to the gas turbine. An increas- ingly popular cooling method uses high-pressure inlet fogging. The performance of a sample of 67 gas turbines augmented with high-pressure inlet fogging was investi- gated in the Journal of Engineering for Gas Turbines and Power (January 2005). One measure of performance is heat rate (kilojoules per kilowatt per hour). Heat rates for the 67 gas turbines are listed in the table below. Suppose that stan- dard gas turbines have heat rates with a standard deviation of 1,500 kJ/kWh. Is there sufficient evidence to indicate that the heat rates of the augmented gas turbine engine are more variable than the heat rates of the standard gas turbine en- gine? Test using a = .05.

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Cooling method for gas turbines. During periods of high
electricity demand, especially during the hot summer
months, the power output from a gas turbine engine can
drop dramatically. One way to counter this drop in power
is by cooling the inlet air to the gas turbine. An increas-
ingly popular cooling method uses high-pressure inlet
fogging. The performance of a sample of 67 gas turbines
augmented with high-pressure inlet fogging was investi-
gated in the Journal of Engineering for Gas Turbines and
Power (January 2005). One measure of performance is heat
rate (kilojoules per kilowatt per hour). Heat rates for the 67
gas turbines are listed in the table below. Suppose that stan-
dard gas turbines have heat rates with a standard deviation
of 1,500 kJ/kWh. Is there sufficient evidence to indicate that
the heat rates of the augmented gas turbine engine are more
variable than the heat rates of the standard gas turbine en-
gine? Test using a = .05.
Transcribed Image Text:Cooling method for gas turbines. During periods of high electricity demand, especially during the hot summer months, the power output from a gas turbine engine can drop dramatically. One way to counter this drop in power is by cooling the inlet air to the gas turbine. An increas- ingly popular cooling method uses high-pressure inlet fogging. The performance of a sample of 67 gas turbines augmented with high-pressure inlet fogging was investi- gated in the Journal of Engineering for Gas Turbines and Power (January 2005). One measure of performance is heat rate (kilojoules per kilowatt per hour). Heat rates for the 67 gas turbines are listed in the table below. Suppose that stan- dard gas turbines have heat rates with a standard deviation of 1,500 kJ/kWh. Is there sufficient evidence to indicate that the heat rates of the augmented gas turbine engine are more variable than the heat rates of the standard gas turbine en- gine? Test using a = .05.
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