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Multi–Disciplinary Optimization for the Conceptual Design of Innovative Aircraft Configurations
Computer Modeling in Engineering & Sciences 2006, 13(1), 1-18. https://doi.org/10.3970/cmes.2006.013.001
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The paper presents an overview of recent work by the authors and their collaborators on multi--disciplinary optimization for conceptual design, based on the integrated modeling of structures, aerodynamics, and aeroelasticity. The motivation for the work is the design of innovative aircraft configurations, and is therefore first--principles based, since in this case the designer cannot rely upon past experience. The algorithms used and the philosophy behind the choices are discussed.Keywords
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APA Style
Morino, L., Bernardini, G., Mastroddi, F. (2006). Multi–disciplinary optimization for the conceptual design of innovative aircraft configurations. Computer Modeling in Engineering & Sciences, 13(1), 1-18. https://doi.org/10.3970/cmes.2006.013.001
Vancouver Style
Morino L, Bernardini G, Mastroddi F. Multi–disciplinary optimization for the conceptual design of innovative aircraft configurations. Comput Model Eng Sci. 2006;13(1):1-18 https://doi.org/10.3970/cmes.2006.013.001
IEEE Style
L. Morino, G. Bernardini, and F. Mastroddi, “Multi–Disciplinary Optimization for the Conceptual Design of Innovative Aircraft Configurations,” Comput. Model. Eng. Sci., vol. 13, no. 1, pp. 1-18, 2006. https://doi.org/10.3970/cmes.2006.013.001
Copyright © 2006 The Author(s). Published by Tech Science Press.This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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