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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 /629/CH12/EX12.8/example12_8.sce | |
| parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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initial commit / add all books
Diffstat (limited to '629/CH12/EX12.8/example12_8.sce')
| -rw-r--r-- | 629/CH12/EX12.8/example12_8.sce | 19 |
1 files changed, 19 insertions, 0 deletions
diff --git a/629/CH12/EX12.8/example12_8.sce b/629/CH12/EX12.8/example12_8.sce new file mode 100644 index 000000000..fa95625a4 --- /dev/null +++ b/629/CH12/EX12.8/example12_8.sce @@ -0,0 +1,19 @@ +clear
+clc
+//Example 12.8 FLOW PROPERTIES IN SUPERSONIC WIND TUNNEL
+k=1.4;
+R=287; //[J/kg.K]
+//From table A.1, interpolating for A/Ao=10,
+M=3.91; //Mach number
+printf("\n The Mach number at the test section, M = %.2f.\n\n",M)
+pt=4000; //pressure[kPa]
+Tt=350; //temp.[K]
+//In test section
+p=0.00743*pt //[kPa]
+T=0.246*Tt //[K]
+printf("\n At the test section, pressure p = %.1f kPa and temperature T = %.f K.\n\n",p,T)
+//Speed of sound
+c=sqrt(k*R*T) //[m/s]
+//Velocity
+V=M*c //[m/s]
+printf("\n The velocity at test section, V = %.f m/s.\n",V)
\ No newline at end of file |