Zobrazeno 1 - 10
of 55
pro vyhledávání: '"Jurij Sodja"'
Publikováno v:
Actuators, Vol 12, Iss 7, p 280 (2023)
This paper proposes an incremental nonlinear control method for an aeroelastic system’s gust load alleviation and active flutter suppression. These two control objectives can be achieved without modifying the control architecture or the control par
Externí odkaz:
https://doaj.org/article/cac722b313324902bcf97f888a655e0a
Autor:
Roeland De Breuker, Tigran Mkhoyan, Nakash Nazeer, Vincent Stuber, Xuerui Wang, Iren Mkhoyan, Roger Groves, Sybrand van der Zwaag, Jurij Sodja
Publikováno v:
Actuators, Vol 11, Iss 10, p 302 (2022)
This article describes the challenges of integrating smart sensing, actuation, and control concepts into an over-sensed and over-actuated technology integrator. This technology integrator has more control inputs than the expected responses or outputs
Externí odkaz:
https://doaj.org/article/0e4ff0a840124ec0a5548afef54b578b
Autor:
Wolf R. Krüger, Yasser M. Meddaikar, Johannes K. S. Dillinger, Jurij Sodja, Roeland De Breuker
Publikováno v:
Aerospace, Vol 9, Iss 10, p 535 (2022)
This article presents the application of aeroelastic tailoring in the design of wings for a flying demonstrator, as well as the validation of the design methodology with flight test results. The investigations were performed in the FLEXOP project (Fl
Externí odkaz:
https://doaj.org/article/5a019dc5ae0645d1a500ff5090b64a0f
Autor:
Xavier Carrillo Córcoles, Christoph Mertens, Andrea Sciacchitano, Bas W. van Oudheusden, Roeland De Breuker, Jurij Sodja
Publikováno v:
Journal of Aircraft. :1-20
This study presents an aeroelastic wind-tunnel experiment to identify the influence of the wing stiffness and hinge release threshold on the gust load alleviation performance of a folding wingtip design. Five models with different stiffness and tailo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1e2cce76d8b5433c0da81e3d1ca56dda
https://doi.org/10.2514/1.c037108
https://doi.org/10.2514/1.c037108
Autor:
Christoph Mertens, José L. Costa Fernández, Jurij Sodja, Andrea Sciacchitano, Bas W. van Oudheusden
Publikováno v:
AIAA Journal. :1-16
The aeroelastic response of the Delft–Pazy wing to steady and periodic unsteady inflow conditions is analyzed experimentally. The Delft–Pazy wing is a highly flexible wing model based on the benchmark Pazy wing (Avin, O., Raveh, D. E., Drachinsky
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6c5d4f7ad3a0b0bc85df07c92b3a7570
https://doi.org/10.2514/1.j062476
https://doi.org/10.2514/1.j062476
Publikováno v:
Actuators; Volume 12; Issue 7; Pages: 280
This paper proposes an incremental nonlinear control method for an aeroelastic system’s gust load alleviation and active flutter suppression. These two control objectives can be achieved without modifying the control architecture or the control par
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=multidiscipl::6ee63d03a452f21ea2bad686b6d2739b
Publikováno v:
AIAA SciTech Forum 2023
In this paper, an innovative design methodology is proposed to simultaneously optimize the size, layout, and number of stiffeners of a stiffened panel using a gradient-based optimizer. In the proposed method, CAD-based parameterization is used to par
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::39d84fe304aacd63ff6636b0ac198ea2
http://resolver.tudelft.nl/uuid:7629c07d-a31b-411e-a266-aada56752e82
http://resolver.tudelft.nl/uuid:7629c07d-a31b-411e-a266-aada56752e82
Publikováno v:
AIAA SciTech Forum 2023
Previous numerical and experimental studies have shown the load alleviation capabilities of the flared folding wingtip. However, they have also shown the complex dynamics of the system and the limitations in the results obtained by modeling such an a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9cb0b40ba8d2aa0a04d76e49bfff7ee7
https://doi.org/10.2514/6.2023-0378
https://doi.org/10.2514/6.2023-0378
Publikováno v:
AIAA SciTech Forum 2023
A new flutter test version of the Parametric Flutter Margin (PFM) method, specifically applied to wings undergoing large deflections is presented. The PFM method adds a stabilising parameter, such as a stabilising mass, to the model such that the flu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::5cb7d531f95002d577e74d8fc7d5a9a6
http://resolver.tudelft.nl/uuid:b0f175ef-b695-49fd-b0ba-755fcd85abd9
http://resolver.tudelft.nl/uuid:b0f175ef-b695-49fd-b0ba-755fcd85abd9
Autor:
Jurij Sodja, Roeland De Breuker
Publikováno v:
AIAA SCITECH 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::98459f9548db683567871ae677032c86
https://doi.org/10.2514/6.2022-2418
https://doi.org/10.2514/6.2022-2418