This two-page review synthesizes and evaluates practical and advanced aerodynamic methods for maximizing an aircraft wing's maximum lift coefficient (CL, max ). The focus is on applications requiring ultra-high lift, such as Short Takeoff and Landing (STOL), Vertical Takeoff and Landing (VTOL), and low-speed heavy-lift operations. Techniques are categorized into three domains: conventional geometric devices (leading-edge slats, Fowler flaps), passive flow manipulators (vortex generators, Gurney flaps), and active/advanced flow control (AFC) (externally blown flaps, circulation control wings, boundary-layer suction). For each method, we delineate the fundamental aerodynamic mechanism, quantify the typical performance payoff, and analyze crucial system-level trade-offs (mass, power consumption, acoustics, and maintenance burden). The paper concludes with a systematic, engineering-oriented design strategy for selecting and integrating these high-lift solutions.