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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 /555/CH1/EX1.1/1.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
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-rw-r--r-- | 555/CH1/EX1.1/1.sce | 16 |
1 files changed, 16 insertions, 0 deletions
diff --git a/555/CH1/EX1.1/1.sce b/555/CH1/EX1.1/1.sce new file mode 100644 index 000000000..725617258 --- /dev/null +++ b/555/CH1/EX1.1/1.sce @@ -0,0 +1,16 @@ +// Implementation of example 1.1
+// Basic and Applied Thermodynamics by P.K.Nag
+// page 20
+clc
+clear
+
+z=562 // (difference in height of mercury in two limbs in mm)
+g=9.79 // (acceleration due to gravity in m/s^2)
+z0=761 // (barometer reading in mm Hg)
+d=13640 // (density of mercury in kg/m^3)
+
+// p= p0 + (d*g*z) & p0=(d*g*z)so
+p=(d*g)*(z+z0)/1000; // division by 1000 is done to convert mm to m
+p=(p/100000); // here division by 100000 is done to convert kPa to atm
+printf("The gas pressure = %.2f bar",p);
+// end
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