| Name: | gr_blade_attack0 - a GRToolbox module |
| Description: | Calculates the thickness of an airfoil. Therefore the area between 2 curves of the same orientation is integrated. The area is calculated using the formula: (x[n+1]-x[n])*(y[n+1]-y[n])/2 nd linear interpolation between two points. |
| Synopsis: | -[chord thicknessh o v noc nof now skip f m c e i s l] -help For help on all options. |
| Special Options: | -chord Prints only the chord. -thickness Prints only the thickness. |
| Example Input Data: | @title gr_blade_attack0: No test data available |
| Example Output Data: | @title gr_blade_attack0: No test data available Back to List of all GR Modules. |