METHODOLOGY FOR THE DESIGN AND EVALUATION OF WING LEADING EDGE AND TRAILING EDGE DEVICES

摘要

This paper presents the development of a methodology for the design and evaluation of wing Leading Edge (LE) and Trailing Edge (TE) devices. This methodology covers the design of such devices, considering different aspects such as mass, reliability, structure and aerodynamic improvements. This paper will present the methodology but also show a case study of its use. The results of this case study will be then discussed and conclusions made.