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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3685/CH5/EX5.5 | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '3685/CH5/EX5.5')
-rw-r--r-- | 3685/CH5/EX5.5/Ex5_5.sce | 21 | ||||
-rw-r--r-- | 3685/CH5/EX5.5/Ex5_5.txt | 6 |
2 files changed, 27 insertions, 0 deletions
diff --git a/3685/CH5/EX5.5/Ex5_5.sce b/3685/CH5/EX5.5/Ex5_5.sce new file mode 100644 index 000000000..d5281e142 --- /dev/null +++ b/3685/CH5/EX5.5/Ex5_5.sce @@ -0,0 +1,21 @@ +clc
+t1 = 15 // Heat exchanger inlet temperature in degree Celsius
+t2 = 800 // Heat exchanger exit temperature in degree Celsius
+t3 = 650 // Turbine exit temperature in degree Celsius
+t4 = 500 // Nozzle exit temperature in degree Celsius
+v1 = 30 // Velocity of steam at heat exchanger inlet in m/s
+v2 = 30// Velocity of steam at turbine inlet in m/s
+v3 = 60 // Velocity of steam at nozzle inlet in m/s
+w = 2 // mass flow rate in kg/s
+cp = 1005 // Specific heat capacity of air in kJ/kgK
+
+printf("\n Example 5.5")
+Q1_2 = w*cp*(t2-t1) // rate of heat transfer
+printf("\n The rate of heat transfer to the air in the heat exchanger is %d kJ/s",Q1_2/1e3)
+
+W_T = w*( ((v2^2-v3^2)/2) + cp*(t2-t3)) // power output from the turbine
+printf("\n The power output from the turbine assuming no heat loss is %f kW",W_T/1000)
+v4 = sqrt( (v3^2) + (2*cp*(t3-t4)) ) // velocity at the exit of the nozzle
+printf("\n The velocity at the exit of the nozzle is %d m/s",v4)
+//The answers vary due to round off error
+
diff --git a/3685/CH5/EX5.5/Ex5_5.txt b/3685/CH5/EX5.5/Ex5_5.txt new file mode 100644 index 000000000..d653fca16 --- /dev/null +++ b/3685/CH5/EX5.5/Ex5_5.txt @@ -0,0 +1,6 @@ +
+
+ Example 5.5
+ The rate of heat transfer to the air in the heat exchanger is 1577 kJ/s
+ The power output from the turbine assuming no heat loss is 298.800000 kW
+ The velocity at the exit of the nozzle is 552 m/s
\ No newline at end of file |