Graphical representation of pair-wise comparison of regression line among different wings from The influence of aspect ratio and stroke pattern on force generation of a bat-inspired membrane wing

Graphical representation of the results of the comparison of the regression slopes for the coefficient of lift and coefficient of drag vs. velocity ratio, computed for different wing models. The horizontal lines illustrate the confidence interval of the pairwise comparisons. Overlap between the confidence intervals of the models indicates that the slopes of the regressions are not significantly different (p > 0.05).