The method involved a meticulous, repetitive procedure designed to analyze wing structures. It focused on subjecting small-scale models of airfoils to controlled stress, meticulously documenting the resulting deformation and failure points. This practical, hands-on technique provided quantitative data about lift and drag characteristics, allowing for incremental refinement of their designs.
Its significance lies in its direct contribution to understanding the relationship between airfoil shape and aerodynamic performance. By systematically testing various wing configurations, valuable empirical data was generated that challenged existing aerodynamic theories and helped develop more efficient and controllable aircraft. This process fostered innovation and ultimately facilitated the successful flight at Kitty Hawk.
