Design, Analysis and Optimization of Composite Wings. Implementation of a211 Composite Wing Sizing Routine in a Multi-Discipline Optimization Program

摘要

This report describes the improvements made on the composite wing sizing routines211u001eof the Multi Model Generator, which is part of the MDO program ('Multi-Discipline 211u001eDesign, Analysis and Optimization of Aerospace vehicles'). The design, analysis 211u001eand optimization of a composite wing structure will be discussed, together with 211u001ethe implementation of the routines in the Multi Model Generator. The new 211u001ecomposite wing sizing routines are, compared to the old ones, more flexible and 211u001eaccurate, handle more design variables and create results that are more 211u001erealistic, taking into account static and static aeroelastic loads, reparability, 211u001emanufacturing, structural stability, damage tolerance, and aeroelastic effects.