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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Maheri, Alireza
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2024Investigating Thermal Dynamic Behavior of Cryogenic Cooling for Low-Energy Impact Fracturing on ISO EN 1.0577 (S355J2) Mild Carbon Steel Grade Offshore Monopile Structures
- 2018Dynamic simulation of machining composites using the explicit element-free Galerkin methodcitations
- 2015Modelling of cutting fibrous composite materials: current practicecitations
- 2015Machining Unidirectional Composites using Single-Point Toolscitations
- 2015Machining Unidirectional Composites using Single-Point Tools: Analysis of Cutting Forces, Chip Formation and Surface Integritycitations
- 2009Upgrading the performance level of ordinary frames using fibre reinforced plastic sheets
- 2008Variable-state design parameters in the design of aero-structures made of intrinsically smart materialscitations
- 2008Variable-state design parameters in design of aero-structures made of intrinsically smart materials
Places of action
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booksection
Variable-state design parameters in the design of aero-structures made of intrinsically smart materials
Abstract
<p>The aerodynamic performance of aero-structures made of intrinsically smart materials, such as aeroelastic tailored wings and blades, cannot be obtained unless their material properties and structural characteristics are also known. The aerodynamic design of these structures is a naturally integrated design problem in which the set of design parameters comprises both aerodynamic and structural characteristics of the aero-structure. This paper references the inevitable problems arising when adopting an integrated design approach, suggesting an alternative approach for design of these structures. The concept of Variable State Design Parameters (VSDP) is introduced in this paper and it is explained how VSDP can be employed to convert the traditional integrated design process of intrinsically smart aero-structures, to a decoupled and hence computationally efficient design process. Through a design case study the practicality and efficiency of the new approach have been demonstrated.</p>