9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization 2002
DOI: 10.2514/6.2002-5447
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Development of an ICAD Generative Model for Blended Wing-Body Aircraft Design

Abstract: Aim of the EC sponsored project 'Multidisciplinary Design and Optimization of Blended Wing-Bodies' is the development and application of a fully integrated Computer Design Engine (CDE). TU Delft contributed to the project with the development of a Blended Wing-Body Multi-Model Generator, which is able to supply geometries and data to the analysis software, either COTS or tailor made, used by the various disciplinary groups in the project team (aerodynamics, structures, stability and control etc.). A full param… Show more

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Cited by 55 publications
(19 citation statements)
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“…The Formal model is described by an object-oriented annotation called MML that is based on UML. The Design and Engineering Engine, DEE, is another approach for the development of knowledge-based engineering applications (La Rocca et al, 2002;Lisandrin and van Tooren, 2002;van Tooren et al, 2003). This approach consists of three major elements: The first element is concerned with the design process, which includes multidisciplinary optimisation.…”
Section: Methods and Models Supporting System Developmentmentioning
confidence: 99%
“…The Formal model is described by an object-oriented annotation called MML that is based on UML. The Design and Engineering Engine, DEE, is another approach for the development of knowledge-based engineering applications (La Rocca et al, 2002;Lisandrin and van Tooren, 2002;van Tooren et al, 2003). This approach consists of three major elements: The first element is concerned with the design process, which includes multidisciplinary optimisation.…”
Section: Methods and Models Supporting System Developmentmentioning
confidence: 99%
“…An example is in the field of robotics systems (Trabelsi et al, 2015), where Chen developed a simple design principle for an untethered, entirely soft, swimming robot with the ability to achieve directional propulsion without batteries and on-board electronics. A multidisciplinary design optimization advisor system (Sobieszczanski-Sobieski et al, 2015) and the implementation of an ICAD generative model (La Rocca et al, 2002) was proposed in the design of aircraft applications. There are numerous methods to solve this kind of problems and many other methods are also studied to improve calculation time and precision in CSP problems.…”
Section: State Of the Artmentioning
confidence: 99%
“…Consider N instances of a parametric CAD geometry, with the corresponding sets of design variables used to control them denoted by [x (1) ,…”
Section: A Preliminariesmentioning
confidence: 99%
“…These tools are often tightly coupled with the meshing and analysis capability of the MDO system and are designed for relatively narrow classes of applications. Increasingly, however, we see commercial parametric CAD packages taking center stage in MDO systems as geometry providers, 1 and this is the perspective we adopt here; nonetheless, much of the following discussion is valid for other forms of geometry construction as well.…”
mentioning
confidence: 99%