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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Klimmek, Thomas
in Cooperation with on an Cooperation-Score of 37%
Topics
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- engine
- modeling
- weight
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- aerodynamic
- structural design
- drone
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- estimating
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- air shipment
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- fuselage
- transport aircraft
- buckling
- aeroelasticity
- simulation
- evolution
- vehicle frame
- gear tooth
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- behavior
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- law
- stiffness
- composite material
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- deformation curve
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- researcher
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- Research Context Victoria
- finite element method
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- show 89 more
Publications (34/34 displayed)
- 2023Parametric aeroelastic modeling, maneuver loads analysis using CFD methods and structural design of a fighter aircraft
- 2022Structural Design of Heavy-Lift Unmanned Cargo Drones in Low Altitudescitations
- 2022A framework for the bi-level optimization of a generic transport aircraft fuselage using aeroelastic loads
- 2022Strukturmodellierung und Lastanalyse eines Mittelstreckenflugzeugs im Projekt ALEGRO
- 2022Aeroelastic method to investigate nonlinear elastic wing structurescitations
- 2022Numerical investigation of power flow input into a fuselage due to jet engine induced wing vibrations
- 2022Aeroelastic Modeling, Loads Analysis and Structural Design of a Fighter Aircraft
- 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
- 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
- 2020Sensitivity-based Multifidelity Multidisciplinary Optimization of a Powered Aircraft Subject to a Comprehensive Set of Loads
- 2020Das DLR-Projekt KonTeKst: Konzepte und Technologien für emissionsarme Kurzstreckenflugzeuge
- 2020Aircraft Loads – A Wide Range of Disciplinary and Process-Related Issues in Simulation and Experiment
- 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
- 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
- 2018Design, Structural Optimization and Loads Assessment for a Flying Wing
- 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”
- 2016Aircraft Loads - An Important Task from Pre-Design to Loads Flight Testing
- 2016A Fully Automatic Structural Optimization Framework to Determine Critical Loads
- 2016Definition of a Comprehensive Loads Process in the DLR Project iLOADS
- 2016Statische aeroelastische Anforderungen beim multidisziplinären Strukturentwurf von Transportflugzeugflügeln
- 2016ALLEGRA Meilensteinbericht M 3.3.3 - Böensimulation des elastischen Flugzeugs mit ROM-Verfahren
- 2015Böenlastanalyse der vorwärts gepfeilten ALLEGRA-Konfiguration
- 2014Design and aeroelastic assessment of a forward-swept wing aircraftcitations
- 2014Parametric Set-Up of a Structural Model for FERMAT Configuration for Aeroelastic and Loads Analysis
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