479.575 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Ziakopoulos, Apostolos | Athens |
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| Vigliani, Alessandro | Turin |
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| Catani, Jacopo | Rome |
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| Statheros, Thomas | Stevenage |
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| Utriainen, Roni | Tampere |
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| Guglieri, Giorgio | Turin |
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| Martínez Sánchez, Joaquín |
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| Tobolar, Jakub |
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| Volodarets, M. |
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| Piwowar, Piotr |
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| Tennoy, Aud | Oslo |
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| Matos, Ana Rita |
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| Cicevic, Svetlana |
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| Sommer, Carsten | Kassel |
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| Liu, Meiqi |
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| Pirdavani, Ali | Hasselt |
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| Niklaß, Malte |
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| Lima, Pedro | Braga |
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| Turunen, Anu W. |
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| Antunes, Carlos Henggeler |
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| Krasnov, Oleg A. |
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| Lopes, Joao P. |
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| Turan, Osman |
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| Lučanin, Vojkan | Belgrade |
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| Tanaskovic, Jovan |
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Schulze, Matthias
German Aerospace Center
in Cooperation with on an Cooperation-Score of 37%
Topics
- engine
- modeling
- weight
- simulation
- flight
- design method
- optimisation
- stiffness
- airplane
- transport aircraft
- pylon
- aircraft
- composite material
- data
- industry
- reliability
- algorithm
- chain
- design
- constraint
- bottleneck
- sensitivity
- passenger
- software
- vehicle occupant
- passenger aircraft
- flexibility
- structural analysis
- wide body aircraft
- assessment
- estimating
- implementation
- surveillance
- aerodynamic
- airfoil
- design load
- researcher
- attention
- civil aircraft
- nacelle
- human being
- commercial transportation
- submarine
- chemical element
- validation
- sea shell
- particle beam
- gust
- variable
- train consist
- geometry
- shipment
- fuselage
- vortex
- structural design
- buckling
- mathematical analysis
- employed
- aeronautics
- aviation
- system architecture
- Research Context Victoria
- finite element method
- pilot study
- iterative method
- static structural analysis
- airframe
- beltway
- regulation
- forecasting
- dynamic model
- structural model
- show 42 more
Publications (22/22 displayed)
- 2021Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integrationcitations
- 2021Loads analysis and structural optimization of a high aspect ratio, composite wing aircraftcitations
- 2021Comparing Two Multidisciplinary Optimization Formulations of Trimmed Aircraft Subject to Industry-relevant Loads and Constraints
- 2021Sensitivity-based Generation of Pareto Fronts for Design of Powered Aircraft Subject to a Comprehensive Set of Loads
- 2021Loads analysis and structural optimization of a high aspect ratio composite wing aircraftcitations
- 2020Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integrationcitations
- 2020Overview of Collaborative Multi-Fidelity Multidisciplinary Design Optimization Activities in the DLR Project VicToriacitations
- 2020Cybermatrix: A novel approach to computationally and collaboration intensive MDO for transport aircraft design
- 2020Sensitivity-based Multifidelity Multidisciplinary Optimization of a Powered Aircraft Subject to a Comprehensive Set of Loads
- 2020The cybermatrix protocol for multidisciplinary optimization of commercial transport aircraft
- 2020High-Fidelity-based MDO: A Closer Look at the Selected Sub-Processes Overall Aircraft Design Synthesis, Loads Analysis, and Structural Optimization
- 2020Cybermatrix protocol: a novel approach to highly collaborative and computationally intensive multidisciplinary aircraft optimization
- 2020A COMPARISON BETWEEN TWO MULTIDISCIPLINARY DESIGN OPTIMIZATION FORMULATIONS FOR TRIMMED TRANSPORT AIRCRAFT
- 2019cpacs-MONA – An independent and in high fidelity based MDO tasks integrated process for the structural and aeroelastic design for aircraft configurations
- 2019The Cybermatrix protocol: a link between classical aircraft design and formal multidisciplinary optimization approaches
- 2019cpacs-MONA – An independent and in high fidelity based MDO tasks integrated process for the structural and aeroelastic design for aircraft configuarations
- 2018Overall Aircraft Design Synthesis, Loads Analysis, and Structural Optimization - Parameterized Disciplinary Sub-Processes within High Fidelity-based Overall Aircraft MDO
- 2018Overview of collaborative high performance computing-based MDO of transport aircraft in the DLR project VicToria
- 2018Overall Aircraft Design Synthesis, Loads Anaysis, and Structural Optimization - Parameterized Disciplinary Sub-Processes within High Fidelity-based Overall Aircraft MDO
- 2017Aero-Structural Optimization of the NASA Common Research Model
- 2017Status of Gradient-based Airframe MDO at DLR; “The VicToria Project”
- 2016A Fully Automatic Structural Optimization Framework to Determine Critical Loads
Places of action
