380.256 PEOPLE
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| Seuring, Stefan |
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| Nor Azizi, S. |
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| Pato, Margarida Vaz |
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| Kölker, Katrin |
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| Huber, Oliver |
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| Király, Tamás |
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| Spengler, Thomas Stefan |
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| Al-Ammar, Essam A. |
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| Dargahi, Fatemeh |
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| Mota, Rui |
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| Mazalan, Nurul Aliah Amirah |
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| Macharis, Cathy | Brussels |
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| Arunasari, Yova Tri |
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| Nunez, Alfredo | Delft |
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| Bouhorma, Mohammed |
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| Bonato, Matteo |
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| Fitriani, Ira |
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| Autor Correspondente Coelho, Sílvia. |
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| Pond, Stephen |
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| Okwara, Ukoha Kalu |
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| Toufigh, Vahid |
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| Campisi, Tiziana | Enna |
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| Ermolieva, Tatiana |
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| Sánchez-Cambronero, Santos |
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| Agzamov, Akhror |
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Voskuijl, Mark
Netherlands Defence Academy
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (16/16 displayed)
- 2021A trim problem formulation for maximum control authority using the Attainable Moment Set geometry
- 2021A Control Allocation approach to induce the center of pressure position and shape the aircraft transient responsecitations
- 2020Active and passive camber morphing for helicopter rotors towards performance improvements in hover and vertical flight
- 2020Trim for Maximum Control Authority using the Attainable Moment Setcitations
- 2020Preliminary Design of a TE Morphing Surface for Rotorcraftcitations
- 2020Numerical and experimental investigation into the aerodynamic benefits of rotorcraft formation flightcitations
- 2019Assessment of Sub-scale Designs for Scaled Flight Testingcitations
- 2019A Thrust-Elevator Interaction Criterion for Aircraft Optimal Longitudinal Controlcitations
- 2019Streamlining Cross-Organizational Aircraft Development: Results from the AGILE Projectcitations
- 2018Hoplite - a conceptual design environment for helicopters incorporating morphing rotor technology
- 2014Evaluation of the simulation results of the GABRIEL concept. Deliverable 4.3
- 2014Control development of a simplified aircraft model to study the GABRIEL concept. Deliverable 4.5
- 2014Test concept development of the GABRIEL concept, Deliverable 4.7
- 2013Simulation technology and simulation of the GABRIEL concept, Deliverable 4.2
- 2011Implementation of a Heterogeneous, Variable-Fidelity Framework for Flight Mechanics Analysis in Preliminary Aircraft Design
- 2010Development and implementation of a novel parametrization technique for multidisciplinary design initialization
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