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| author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
|---|---|---|
| committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
| commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
| tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3720/CH3/EX3.3/Ex3_3.sce | |
| parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '3720/CH3/EX3.3/Ex3_3.sce')
| -rw-r--r-- | 3720/CH3/EX3.3/Ex3_3.sce | 18 |
1 files changed, 18 insertions, 0 deletions
diff --git a/3720/CH3/EX3.3/Ex3_3.sce b/3720/CH3/EX3.3/Ex3_3.sce new file mode 100644 index 000000000..2c6170e48 --- /dev/null +++ b/3720/CH3/EX3.3/Ex3_3.sce @@ -0,0 +1,18 @@ +// Example 3_3
+clc;clear;funcprot(0);
+// Constants used
+g=9.81;//The acceleration due to gravity in m/s^2
+
+// Given values
+h=1400;//m
+h_1=0.1;//m
+h_2=0.2;//m
+h_3=0.35;// respective heights in m
+P_atm=85.6; // The atmosphereic pressure in kPa;
+rho_w=1000;// kg/m^3
+rho_o=850;// kg/m^3
+rho_m=13600; // The density of water, mercury and oil in kg/m^3
+
+// Calculation
+P_1=P_atm+((rho_m*g*h_3)-(rho_w*g*h_1)-(rho_o*g*h_2))/1000;
+printf('The air pressure in the tank P_1=%0.0fkPa\n',P_1);
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