Moerland, Erwin and Becker, Richard-Gregor and Nagel, Björn (2015) Collaborative understanding of disciplinary correlations using a low-fidelity physics-based aerospace toolkit. CEAS Aeronautical Journal, 6 (3), pp. 441-454. Springer. doi: 10.1007/s13272-015-0153-4. ISSN 1869-5582.
Full text not available from this repository.
Official URL: http://dx.doi.org/10.1007/s13272-015-0153-4
Abstract
When performing aircraft design, covering all relevant physical effects and mutual interactions at a sufficient level of fidelity necessitates simultaneous consideration of a large number of disciplines. This requires methods in which teams of engineers simultaneously apply both their analysis modules and knowledge to collaboratively approach design challenges.
In the current work, recent technical advancements of
the German Aerospace Center (DLR) in data and workflow
management are utilised to establish a toolbox containing
elementary disciplinary analysis modules. This toolbox is
focused on providing fast overall aircraft design capabilities.
The incorporated empirical and physics-based lowfidelity
modules can be used for setting up modular design
workflows, tailored for the considered design cases. This
enables the involved engineers to identify design trends at
low computational effort. Furthermore, areas of common
physical affinity are identified among the engineers, serving
as basis for communication. Clear visualisation methods
aid in efficiently translating knowledge between the
involved engineers within the identified areas of common
affinity. In later phases of the design process, the gathered
knowledge serves as basis for incorporating modules of
higher fidelity.
Two application cases guide the present work. In the
first application case, a system-of-systems approach is
established by applying the elementary aircraft design
toolbox to generate requirement sets for engine preliminary
design. In this way, a clear synergy is established between
the design of both the airframe and power plant. In the
second application case, the applicability of a strut-braced
wing as potential short-to-medium-range aircraft is investigated
by a team of engineers. Within both application
cases, methods are applied in which the involved engineers
share their knowledge through a collaborative design
approach.
| Item URL in elib: | https://elib.dlr.de/102618/ | ||||||||||||||||
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| Document Type: | Article | ||||||||||||||||
| Title: | Collaborative understanding of disciplinary correlations using a low-fidelity physics-based aerospace toolkit | ||||||||||||||||
| Authors: |
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| Date: | 29 April 2015 | ||||||||||||||||
| Journal or Publication Title: | CEAS Aeronautical Journal | ||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||
| Open Access: | No | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||
| Volume: | 6 | ||||||||||||||||
| DOI: | 10.1007/s13272-015-0153-4 | ||||||||||||||||
| Page Range: | pp. 441-454 | ||||||||||||||||
| Publisher: | Springer | ||||||||||||||||
| ISSN: | 1869-5582 | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | Collaborative design, Multidisciplinary design and optimisation, Knowledge management, CPACS, RCE | ||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||||||
| DLR - Research theme (Project): | L - Concepts and Integration (old), L - Simulation and Validation (old) | ||||||||||||||||
| Location: | Hamburg | ||||||||||||||||
| Institutes and Institutions: | Air Transport Operations > Integrated Aircraft Design Institute of Propulsion Technology > Engine | ||||||||||||||||
| Deposited By: | Moerland, Erwin | ||||||||||||||||
| Deposited On: | 28 Jan 2016 10:47 | ||||||||||||||||
| Last Modified: | 16 Sep 2025 04:13 |
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