467.600 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Serhiienko, Serhii |
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| Schmalz, Ulrike |
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| Oliveira, Marisa |
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| Ribeiro Pereira, Maria Teresa |
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| Bellér, Gábor |
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| Araujo, M. |
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| Frey, Michael | Karlsruhe |
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| Coutinho-Rodrigues, João | Coimbra |
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| Wouters, Christian Guillaume Louise | Aachen |
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| Kessel, Paul J. Van Van |
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| Árpád, István |
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| Fontul, Simona |
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| Kocsis, Dénes |
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| Cigada, Alfredo | Milan |
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| Oort, Neils Van | Delft |
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| Agárdi, Anita | Miskolc |
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| Andrews, Gordon E. |
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| Sousa, Nuno |
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| Witlox, Frank Jacomina Albert | Ghent |
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| Dobruszkes, Frederic |
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| Kiss, Judit T. |
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| Hadachi, Amnir | Saint-Étienne-du-Rouvray |
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| Hamilton, Carl J. | Kunovice |
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| Misiura, Serhii |
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| Schimpf, Marina |
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Schütte, Andreas
in Cooperation with on an Cooperation-Score of 37%
Topics
- physics
- behavior
- topology
- design
- geometry
- leading edge
- airplane
- aerodynamic
- vortex
- angle of attack
- assessment
- aircraft
- engine
- specification
- performance evaluation
- design team
- defense
- transport aircraft
- research project
- vehicle frame
- sensitivity
- data
- modeling
- forecasting
- simulation
- design method
- tunnel
- wind tunnel
- wind
- fluid
- amphetamine
- validation
- fuselage
- turbulence
- atmospheric turbulence
- variable
- mach number
- physical property
- nose
- boundary layer separation
- age
- casting
- examination
- flow field
- flood plain
- trailing edge
- experiment
- fluidics
- control device
- laboratory
- coding system
- deflection
- yaw
- estimating
- repairing
- vehicle design
- dynamic stability
- center of gravity
- estimate
- layout
- aerodynamic stability
- sea
- ocean
- flight
- profit
- Reynolds number
- radar
- industry
- evolution
- prototype
- countermeasure
- maneuverability
- employed
- equation
- show 44 more
Publications
- 2022Impact of Planform and Control Surfaces on the Vortical Flow Topology and Roll Stability of a Multi Delta Wing Configurationcitations
- 2022NATO STO/AVT-251: A Joint Exercise in Collaborative Combat Aircraft Design
- 2022DLR Projekt Diabolo: Technologien und Entwurf von Kampfflugzeugen der nächsten Generation
- 2020Multi-Disciplinary Design and Performance Assessment of Effective, Agile NATO Air Vehiclescitations
- 2020Design studies and multi-disciplinary assessment of agile and highly swept flying wing configurations
- 2018Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summarycitations
- 2018DESIGN STUDIES AND MULTI-DISCIPLINARY ASSESSMENT OF AGILE AND HIGHLY SWEPT FLYING WING CONFIGURATIONS
- 2018Computational Aerodynamic Sensitivity Studies for Generic Delta Wing Planforms
- 2017Numerical Investigations of Vortical Flow on Swept Wings with Round Leading Edgescitations
- 2017Untersuchung alternativer Steuerkonzepte für eine Giersteuerung ohne Seitenleit-werk an einer hoch gepfeilten Nurflügelkonfiguration
- 2016Multidisciplinary design and aerodynamic assessment of an agile and highly swept aircraft configurationcitations
- 2016Luftstreitkräfte der Zukunft – Technologische Herausforderungen und Entwurf zukünftiger bemannter sowie unbemannter Kampfflugzeuge
- 2016Stability and Control Investigations of Generic 53 Degree Swept Wing with Control Surfacescitations
- 2016Numerical investigations of the vortical flow on swept wings with round leading edgescitations
- 2016Aerodynamics and Conceptual Design Studies on an Unmanned Combat Aerial Vehicle Configurationcitations
- 2015Numerische aerodynamische Analyse und Bewertung einer agilen und hoch gepfeilten Flugzeugkonfiguration
- 2015Multidisciplinary Design and Aerodynamic Assessment of an Agile and Highly Swept Aircraft Configuration
- 2014Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices
- 2014UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities
- 2012Numerical Investigation of the Aerodynamic Properties of a Flying Wing Configuration
- 2009Untersuchungen von UAV Technologien im DLR
- 2008Numerical investigations on the VFE-2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code
Places of action
