479.575 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Ziakopoulos, Apostolos | Athens |
|
| Vigliani, Alessandro | Turin |
|
| Catani, Jacopo | Rome |
|
| Statheros, Thomas | Stevenage |
|
| Utriainen, Roni | Tampere |
|
| Guglieri, Giorgio | Turin |
|
| Martínez Sánchez, Joaquín |
| |
| Tobolar, Jakub |
| |
| Volodarets, M. |
| |
| Piwowar, Piotr |
| |
| Tennoy, Aud | Oslo |
|
| Matos, Ana Rita |
| |
| Cicevic, Svetlana |
| |
| Sommer, Carsten | Kassel |
|
| Liu, Meiqi |
| |
| Pirdavani, Ali | Hasselt |
|
| Niklaß, Malte |
| |
| Lima, Pedro | Braga |
|
| Turunen, Anu W. |
| |
| Antunes, Carlos Henggeler |
| |
| Krasnov, Oleg A. |
| |
| Lopes, Joao P. |
| |
| Turan, Osman |
| |
| Lučanin, Vojkan | Belgrade |
|
| Tanaskovic, Jovan |
|
Klimmek, Thomas
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- engine
- modeling
- weight
- flight
- optimisation
- aerodynamic
- structural design
- drone
- commodity
- assessment
- estimating
- chemical element
- altitude
- air shipment
- structural model
- cargo aircraft
- air drop
- design method
- submarine
- constraint
- bottleneck
- fuselage
- transport aircraft
- buckling
- aeroelasticity
- simulation
- evolution
- vehicle frame
- gear tooth
- driver
- train consist
- behavior
- design
- law
- stiffness
- composite material
- particle beam
- deformation curve
- bending moment
- noise
- passenger
- vehicle occupant
- vibration
- chain
- transient
- passenger aircraft
- generator
- electric power transmission
- jet propelled aircraft
- jet engine
- gust
- pylon
- structural part
- pressure
- consensus
- airplane
- sensitivity
- software
- flexibility
- structural analysis
- wide body aircraft
- researcher
- industry
- algorithm
- attention
- civil aircraft
- nacelle
- landing
- takeoff
- airport
- motivation
- aeronautics
- ground handling
- aviation
- system architecture
- examination
- layout
- experiment
- implementation
- validation
- sea shell
- airfoil
- design load
- data
- variable
- geometry
- shipment
- vortex
- mathematical analysis
- Research Context Victoria
- finite element method
- pilot study
- iterative method
- static structural analysis
- airframe
- beltway
- physics
- park and ride
- flight test
- regulation
- forecasting
- dynamic model
- vehicle fleet
- definition
- certification
- specification
- voltage
- flood plain
- read only memory
- licensing
- formula
- fuel consumption
- fuel
- dynamic load
- stabiliser
- workshop
- geometric design
- aileron
- show 89 more
Publications
- 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
Places of action
