Approximate Modelling and Multi Objective Optimisation in Aeronautic Design

Vankan, W.J.; Maas, R.

doi:10.3233/jcm-2003-3309

Cited by 3 publications

(1 citation statement)

References 3 publications

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“…Not only the product but also the process information is stored in CPACS. Another example of using the model-based system engineering (MBSE) approach is the AGILE 4.0 project, which also builds ontologies that organise information resources in the aviation field [10,11]. The recipients of these systems are large aviation companies that achieve particular benefits because of the need to exchange information with their co-operators.…”

Section: Methodsmentioning

confidence: 99%

Integrated Aircraft Design System Based on Generative Modelling

Skarka,

Nalepa,

Musik

2023

Aerospace

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This article presents the effects of work performed during a software project for generative models and spreadsheets, allowing the quick creation of conceptual models for aircraft. The presented software at the current stage is suitable for the creation of glider representation; however, a modular structure allows for developing and extrapolating the presented application to match the requirements of planes and UAV (unmanned aerial vehicle) design. The subject of this work is a response to the current trends and needs prevailing in the field of CAD (computer-aided design) and aviation. In the initial sections of this paper, theoretical issues related to the work being carried out are introduced, and the methodology for creating software for the construction and verification of the aircraft structure along with the need for interchange between databases of generative models is presented. In the following sections, the concepts and selected solutions for the user interface that supports the knowledge base are presented along with a set of procedures for its operation. Furthermore, a method for database integration with the methods used to determine design features for the developed generative models and the Siemens NX system is introduced. Problems encountered during software development, as well as solution examples for model applications, are specified. The results obtained and the models generated on their basis were tested with a strength analysis using Autodesk Inventor software and analysed in terms of meeting the initial assumptions. In the end, conclusions and observations were formulated resulting from the effects of the work performed during the project.

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Section: Methodsmentioning

confidence: 99%

Integrated Aircraft Design System Based on Generative Modelling

Skarka,

Nalepa,

Musik

2023

Aerospace

View full text Add to dashboard Cite

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Multiobjective optimization techniques applied to engineering problems

Oliveira¹,

Saramago²

2010

J. Braz. Soc. Mech. Sci. & Eng.

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Integrated Design System of Aircrafts Based on Generative Modeling Method

Skarka,

Nalepa,

Musik

2023

Preprint

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This thesis presents the effects of work done on a software project for generative models and spreadsheets, allowing for a quick creation of the conceptual model of the aircraft. The subject of the work is a response to the current trends and needs prevailing in the field of computer design engineering CAD and aviation. In the initial chapters, theoretical issues related to the work being carried out were introduced and the methodology of creating software for construction and verification of the structure of aircraft along with the needs of interchange between databases of generative models was presented. In the next stages, the concepts and selected solutions for the user interface supporting the knowledge base were presented along with a set of procedures for its operation. Furthermore, the method of database integration with the methods of determining design features for the developed generative models and with the Siemens NX system. Furthermore, problems encountered in software development, as well as solution examples for model application are specified. The results obtained and the models generated on their basis were subjected to a strength analysis using Autodesk Inventor software and analysed in terms of meeting the initial assumptions. In the end, conclusions and observations resulting from the effects of the work presented in the project were formulated.

show abstract

Approximate Modelling and Multi Objective Optimisation in Aeronautic Design

Cited by 3 publications

References 3 publications

Integrated Aircraft Design System Based on Generative Modelling

Integrated Aircraft Design System Based on Generative Modelling

Multiobjective optimization techniques applied to engineering problems

Integrated Design System of Aircrafts Based on Generative Modeling Method

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