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Diffstat (limited to '548/DEPENDENCIES/4_12data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/4_12data.sci | 9 |
1 files changed, 9 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/4_12data.sci b/548/DEPENDENCIES/4_12data.sci new file mode 100755 index 000000000..49ec49944 --- /dev/null +++ b/548/DEPENDENCIES/4_12data.sci @@ -0,0 +1,9 @@ +//Nozzle flow was described in example 4.9,so we can take data from eg 4.9
+V1=580 //velocity at throat,m/s
+Ve=1188 //velocity at exit,m/s
+T1=833 //Temperature at throat,in Kelvin
+Te=300 //Temperature at exit,in kelvin
+R=287;//gas constant for air,J/Kg.K
+y=1.4;// specific heat ratio for air
+a=(y*R*T1)^0.5 //speed of sound at throat
+Ae=(y*R*Te)^0.5 //speed of sound at exit
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