01 - Aircraft Design and Integrated Systems
FAST ITERATIVE SIMULATION OF AIRLINER WING PLANFORM CONCEPTUAL DESIGN
C. Ma¹, Z.Y. Chen¹, C.H. Kong¹; ¹Shanghai Aircraft Design and Research Institute, China
This article illustrates the fast iterative simulation process of wing planform conceptual design. The whole process is built on simplified numerical simulation, based on validated CFD, FEM and CSD methods. There are three main data flow in this process: aerodynamics, weight and rigidity requirements. The variation of wing aspect ratio is investigated to show the multidisciplinary influence.