diff options
| author | priyanka | 2015-06-24 15:03:17 +0530 |
|---|---|---|
| committer | priyanka | 2015-06-24 15:03:17 +0530 |
| commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
| tree | ab291cffc65280e58ac82470ba63fbcca7805165 /548/DEPENDENCIES/5_10_data.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/5_10_data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/5_10_data.sci | 4 |
1 files changed, 4 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/5_10_data.sci b/548/DEPENDENCIES/5_10_data.sci new file mode 100755 index 000000000..db2cfaa26 --- /dev/null +++ b/548/DEPENDENCIES/5_10_data.sci @@ -0,0 +1,4 @@ +//consider a NACA-0012 airfoil
+Cpomin=-0.43;//minimum pressure coefficient on the surface of airfoil at low speed from figure of Cp vs x/c given in question.
+M=linspace(0.4,0.9,6);//Mach number over which we have to calculate Cp critical.
+y=1.4;//specific heat ratio for air.
\ No newline at end of file |