Combined structural and manufacturing optimization of stiffened composite panels

Citation
Jl. Henderson et al., Combined structural and manufacturing optimization of stiffened composite panels, J AIRCRAFT, 36(1), 1999, pp. 246-254
Citations number
32
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF AIRCRAFT
ISSN journal
00218669 → ACNP
Volume
36
Issue
1
Year of publication
1999
Pages
246 - 254
Database
ISI
SICI code
0021-8669(199901/02)36:1<246:CSAMOO>2.0.ZU;2-D
Abstract
Manufacturing considerations have been incorporated into the design optimiz ation of a blade-stiffened composite panel. For the manufacturing analysis, a one-dimensional resin film infusion model is developed to compute the in filtration time of the resin into a fabric preform of the panel. Results ar e presented showing the effects of design variables that are important for structural performance, such as cross-sectional geometry variables and mate rial properties, on the panel manufacturing effort. In addition, the effect s of manufacturing process variables, such as pressure and temperature, on the structural performance are studied. The structural problem is formulate d to minimize the panel mass subject to buckling constraints. A simplified buckling analysis model for the panel is used to compute the critical buckl ing loads. The objective of the manufacturing problem is to minimize the re sin infiltration time. Optimum panel designs for the manufacturing and stru ctures problems alone, as well as for the combined problem, are generated u sing a genetic algorithm. The results indicate a strong connection between the structural and manufacturing design variables and tradeoffs between the two responses, and illustrate that a multidisciplinary approach to the pro blem is essential to incorporate manufacturing into the preliminary design stage.