| Name: | gr_blade_camber - a GRToolbox module |
| Description: | Calculates the camber line, thickness and camber distribution of an airfoil. The algorithm used for this is a predictor corrector algorithm 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: | -[eps camber thickness distributionh o v noc nof now skip f m c e i s l] -help For help on all options. |
| Special Options: | -all Print all values in a single set using 8 columns. Column 1: Camberline x-value. Column 2: Camberline y-value. Column 3: Camberline thickness-value. Column 4: Camberline distribution. Column 5: Normal of camber x coordinate. Column 6: Normal of camber y coordinate. Column 7: Profile coordinate upper side x. Column 8: Profile coordinate upper side y. Column 9: Profile coordinate lower side x. Column 10: Profile coordinate lower side y. -ct Print the camber and thickness in two sets line. -camber Print the camber line. -eps double Accuracy for difference in distance from camberlinne. -distribution Print the camber distribution. -info Print number of points per side. -thickness Print the thickness. |
| Example Input Data: | @title gr_blade_camber: No test data available |
| Example Output Data: | @title gr_blade_camber: No test data available Back to List of all GR Modules. |