Development and application of multi-disciplinary optimization capabilities based on high-fidelity methods
Brezillon, Joel and Ronzheimer, Arno and Haar, Danil and Abu-Zurayk, Mohammad and Lummer, Markus and Krüger, Wolf-Reiner and Natterer, Franz Josef (2012) Development and application of multi-disciplinary optimization capabilities based on high-fidelity methods. 8th AIAA Multidisciplinary Design Optimization Specialist Conference, 23-26 Apr. 2012, Honolulu, Hawaii.
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The expected computational power that will become available in the next years and decades will allow the introduction of more accurate simulations at earlier aircraft design stages. It is thus mandatory to identify and consequently develop multi-disciplinary optimization capabilities based on high-fidelity methods enabling the design of the future aircraft. The paper will give an overview of the latest development conducted at DLR in this field. Three representative applications will demonstrate benefits and limitations of the capabilities developed.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Development and application of multi-disciplinary optimization capabilities based on high-fidelity methods|
|Keywords:||MDO, CATIA V5, CFD, CSM, Wing Design, Engine integration, optimization, Adjoint, Flight Shape, Gradient-based Optimization|
|Event Title:||8th AIAA Multidisciplinary Design Optimization Specialist Conference|
|Event Location:||Honolulu, Hawaii|
|Event Type:||international Conference|
|Event Dates:||23-26 Apr. 2012|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||L AR - Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Flight Physics|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Joel Brezillon|
|Deposited On:||11 Jun 2012 09:48|
|Last Modified:||11 Jun 2012 09:48|
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