Installation of IBL program on PC
1. Go to directory on this CD: document\pan-ibl\IBL Window Package
2. Run the setup.exe program to start installation the package.
Execute the IBL program on your PC
Choose IBL from Start, Programs, Panel-IBL to run IBL program
1. Start execute the IBL program (window)
2. Open geometry input file
3. Select input file which contains airfoil geometry, the number of angles of attack
N, Mach and Reynolds numbers.
4. You can change the number of angles attack, range of angles, Mach and Reynolds
numbers. The output file names can also be changed.
5. Click Calculation from Computation menu
6. Show results in plot by selecting from Show menu
7. You can print or copy the plot to Microsoft Word file.
Mach = 0.1 Reynolds = 4000000
1.6
1.4
1.2
1.0
0.8
0.6
0.4
0.2
2
4
6
8
10
Attack Angle
12
14
16
18
Mach = 0.1 Reynolds = 4000000
-0.05
2
4
6
8
10
-0.10
-0.15
-0.20
-0.25
-0.30
-0.35
Attack Angle
12
14
16
18
8. Exit the program