Study for the Optimization of a Transport Aircraft Wing for Maximum Fuel Efficiency. Volume 1: Methodology, Criteria, Aeroelastic Model Definition and Results

摘要

Work performed in the design of a transport aircraft wing for maximum fuel efficiency is documented with emphasis on design criteria, design methodology, and three design configurations. The design database includes complete finite element model description, sizing data, geometry data, loads data, and inertial data. A design process which satisfies the economics and practical aspects of a real design is illustrated. The cooperative study relationship between the contractor and NASA during the course of the contract is also discussed.