Zobrazeno 1 - 10 of 17 pro vyhledávání: '"Mohammad Abu-Zurayk"'
1
Development of a medium/long-haul reference aircraft
Autor: Benjamin M. H. J. Fröhler, Jannik Häßy, Mohammad Abu-Zurayk
Publikováno v: CEAS Aeronautical Journal.
For the evaluation of future aircraft architectures or novel technologies, a well-understood and sound reference to compare to is essential to prove the impact of intended changes. A reference aircraft serves as a basis for calibration of the aircraf
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8cde15f27b553215e64d88ee543fb97b
https://doi.org/10.1007/s13272-023-00662-1
Zobrazit plný text záznamu
5
Sensitivity-based Multifidelity Multidisciplinary Optimization of a Powered Aircraft Subject to a Comprehensive Set of Loads
Autor: Stefan Görtz, Johannes Hartmann, Jannik Häßy, David Quero-Martin, Stefan Keye, Matthias Schulze, Richard-Gregor Becker, Andrei Merle, Benjamin Fröhler, Thomas Klimmek, Christoph Kaiser, Mohammad Abu-Zurayk, Caslav Ilic
Publikováno v: AIAA AVIATION 2020 FORUM.
Over the past decade, profound attention was given to exploring the benefits of engaging numerical multidisciplinary design optimization in aircraft design. Due to its importance, aerostructural wing design optimization is the most visited multidisci
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::931c4dbc1a2074ab26b111c98fe8031a
https://doi.org/10.2514/6.2020-3168
Zobrazit plný text záznamu
7
Cybermatrix: A Novel Approach to Computationally and Collaboration Intensive Multidisciplinary Optimization for Transport Aircraft Design
Autor: Andrei Merle, Matthias Schulze, Sebastian Gottfried, Arno Ronzheimer, Michael Petsch, Martin Leitner, Mohammad Abu-Zurayk, Jonas Jepsen, Andreas Schuster, Caslav Ilic
Publikováno v: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783030252526
This paper presents an approach to multi-disciplinary optimization (MDO) of transport aircraft that attempts to strike a balance between two broad classes of MDO approaches: those arising from the formal optimization background, and those coming from
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::318b39142d9a1fda11a1adc6e7b59576
https://doi.org/10.1007/978-3-030-25253-3_4
Zobrazit plný text záznamu
8
Surrogate-Based Aerodynamic Shape Optimization of a Wing-Body Transport Aircraft Configuration
Autor: Caslav Ilic, Mohammad Abu-Zurayk, Zhong-Hua Han, Stefan Görtz
Publikováno v: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319720197
Aerodynamic shape optimization driven by high-fidelity computational fluid dynamics (CFD) simulations is still challenging, especially for complex aircraft configurations. The main difficulty is not only associated with the extremely large computatio
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6d24e23170e18834ac62b4dad2968b2e
https://doi.org/10.1007/978-3-319-72020-3_16
Zobrazit plný text záznamu
9
Aero-Structural Optimization of the NASA Common Research Model
Autor: Stefan Keye, Matthias Schulze, Thomas Klimmek, Mohammad Abu-Zurayk, Caslav Ilic
Publikováno v: 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
A combined aerodynamic and structural, gradient-based optimization has been performed on the NASA/Boeing Common Research Model civil transport aircraft configuration. The computation of aerodynamic performance parameters includes a Reynolds-averaged
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4e9ae31f4d8d5beb077daf75abc54476
https://doi.org/10.2514/6.2017-4145
Zobrazit plný text záznamu
10
Comparison of Breguet and ODE Evaluation of the Cruise Mission Segment in the Context of High-Fidelity Aircraft MDO
Autor: Martin Kruse, Tanja Führer, Richard-Gregor Becker, Jan Himisch, Caslav Ilic, Gunnar Einarsson, Doreen Seider, Nagaraj Banavara, Mohammad Abu-Zurayk
Publikováno v: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ISBN: 9783319272788
This report presents a multi-disciplinary optimization (MDO) process that minimizes the mission fuel burn of an aeroelastic long-range transport aircraft configuration, by modifying the wing planform, twist, and structural element thicknesses. Two op
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::662cc6c0efced752dcd76840681bebcd
https://doi.org/10.1007/978-3-319-27279-5_8
Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání

Omezení vyhledávání
Plný text Recenzováno Digitální knihovna AV ČR
Zdroje