02.4 - Applied AerodynamicsIMPROVED DESIGN OF A HIGH LIFT SYSTEM FOR GENERAL AVIATION AIRCRAFTD. Florjancic¹, D. Steenhuizen¹, L.L.M. Veldhuis¹; ¹TU Delft, Netherlands Optimization of a single slotted flap is performed with the objective of increasing payload of a general aviation aircraft. Within the optimization loop, two-dimensional aerodynamic characteristics are evaluated using the MSES code, while three-dimensional aerodynamic characteristics and weight are estimated with semi-empirical methods. It is found that the payload can be increased by up to 40%. |