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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 /3785/CH12/EX12.3/Ex12_3.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '3785/CH12/EX12.3/Ex12_3.sce')
-rw-r--r-- | 3785/CH12/EX12.3/Ex12_3.sce | 10 |
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diff --git a/3785/CH12/EX12.3/Ex12_3.sce b/3785/CH12/EX12.3/Ex12_3.sce new file mode 100644 index 000000000..f80edcbc5 --- /dev/null +++ b/3785/CH12/EX12.3/Ex12_3.sce @@ -0,0 +1,10 @@ +// Example 12_3
+clc;funcprot(0);
+// Given data
+r=1.4;// The specific heat ratio
+p_s=6*10^5;// The pressure in the large tank in Pa
+p_t=5*10^4;// The pressure in the test section in Pa
+
+// Calculation
+M_t=sqrt((2/(r-1))*((p_t/p_s)^(-(r-1)/r)-1));// Mach number
+printf("\nThe Mach number M_t in the test section is %1.3f",M_t);
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