10.01.2015 Views

Chapter 13 Gas Turbine Power Plants

Chapter 13 Gas Turbine Power Plants

Chapter 13 Gas Turbine Power Plants

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

Problems<br />

<strong>13</strong>.1 Write the expression for the net work of the ideal Brayton<br />

cycle. Show by differentiation that the W net is maximum when<br />

-*02 = "V 01 03<br />

<strong>13</strong>.2 Use the optimum temperature T 02 found in Problem <strong>13</strong>.1 to<br />

determine the corresponding optimum cycle pressure ratio for the<br />

ideal Brayton cycle.<br />

<strong>13</strong>.3 Write the expression for the turbine work of the ideal Brayton<br />

cycle in terms of T 03 and r p . Use the result to conclude how<br />

the turbine work can be increased by changing these quantities.<br />

<strong>13</strong>.4 Write the expression for the compressor work of the ideal<br />

Brayton cycle in terms of T ol and r p . Use the result to conclude<br />

how the compressor work can be decreased by changing these<br />

quantities.<br />

<strong>13</strong>.5 An ideal Brayton cycle uses air as the working substance.<br />

At the compressor inlet p 01 = 1 atm and T 0! = 294°K,, and at the<br />

turbine inlet p 03 =12 atm and T 03 = 1222°K. The mass flow rate<br />

of air is 11.33 kg/s. Assuming that y has a constant value of 1.4,<br />

determine the cycle efficiency and the net power developed.<br />

<strong>13</strong>.6 An ideal Brayton cycle uses air as the working substance.<br />

At the compressor inlet p 01 = 1 atm and T 01 = 294°K, and at the<br />

turbine inlet p 03 =12 atm and T 03 = 1222°K. The mass flow rate<br />

of air is 11.33 kg/s. Assuming that y varies with average temperature<br />

in each process and using (11.5), determine the cycle efficiency<br />

and the net power developed<br />

<strong>13</strong>.7 A Brayton cycle uses air as the working substance. At the<br />

compressor inlet p 0 i = 1 atm and T 01 = 300°K, and at the turbine

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!