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| author | priyanka | 2015-06-24 15:03:17 +0530 |
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| committer | priyanka | 2015-06-24 15:03:17 +0530 |
| commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
| tree | ab291cffc65280e58ac82470ba63fbcca7805165 /548/DEPENDENCIES/4_07data.sci | |
| download | Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.gz Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.bz2 Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.zip | |
initial commit / add all books
Diffstat (limited to '548/DEPENDENCIES/4_07data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/4_07data.sci | 8 |
1 files changed, 8 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/4_07data.sci b/548/DEPENDENCIES/4_07data.sci new file mode 100755 index 000000000..7d6069dff --- /dev/null +++ b/548/DEPENDENCIES/4_07data.sci @@ -0,0 +1,8 @@ +//An airplane is flying at standard sea level condition.
+//The flow conditions are assumed to be isentropic in nature.
+T=250;//temperature at a point on wing in Kelvin
+P1=1.01*10^5;//pressure at far upstream of wing
+T1=288.16;//temperature at far upstream of wing
+y=1.4;//ratio of specific heats for air
+
+
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