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OPTIMOrph

Development of methods for deriving optimized shapes of morphing structures considering both aerodynamic performances and specific mechanical morphing boundary conditions

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

OPTIMOrph project word cloud

Explore the words cloud of the OPTIMOrph project. It provides you a very rough idea of what is the project "OPTIMOrph" about.

aerodynamic proof material actually reconstruction mechanical optimization effort complexity drag procedure mechanisms edge constrained considerations indications shapes limitations gas solutions positions implementing basically fsi keeping compliant industrial re disciplinary optimorph model pertinent either engineering lift engine feasibility upcoming structural limits acceptable accurate wing optimal inclusion unprecedented architectures assist series turn operators completely surrogate consideration stages structures requirement aircraft materials methodology featuring deflected technologies computational solver morphing fidelity delivered performance numerical consistent

Project "OPTIMOrph" data sheet

The following table provides information about the project.

Coordinator	HIT09 SRL Organization address address: PIAZZETTA BETTIOL GIUSEPPE 15 city: PADOVA PD postcode: 35137 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Italy [IT]
Total cost	350˙725 €
EC max contribution	350˙725 € (100%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP04-2016-02
Funding Scheme	CS2-RIA
Starting year	2017
Duration (year-month-day)	from 2017-06-01 to 2019-06-30

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	HIT09 SRL HIT09 SRL Organization address address: PIAZZETTA BETTIOL GIUSEPPE 15 city: PADOVA PD postcode: 35137 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (PADOVA PD)	coordinator	236˙850.00
2	SWANSEA UNIVERSITY SWANSEA UNIVERSITY Organization address address: SINGLETON PARK city: SWANSEA postcode: SA2 8PP website: www.swan.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (SWANSEA)	participant	113˙875.00

Map

Project objective

The OPTIMOrph project addresses the development of a robust and reliable numerical optimization methodology able to identify target shapes for deflected positions of morphing structures based on optimal aerodynamic characteristics (i.e. basically lift and drag), while taking into account in a consistent way feasibility issues related to mechanical considerations and material properties. This is actually a requirement very specific to morphing structures, where the mechanical feasibility and complexity is one of the key features to be taken into consideration throughout the design process. The project objectives will be achieved through the implementation of a general multi-disciplinary, multi-objective, multi-constrained optimization procedure able to enhance aerodynamic performance in a compliant way with the pertinent morphing mechanisms and materials limitations, thus enabling the implementation of a step-change in the design of morphing structures. In OPTIMOrph, a multi-fidelity approach will be adopted, in which a high-fidelity FSI solver will be used for reconstruction of a surrogate model (low-fidelity), which in turn will assist a very advanced optimization engine where GAs featuring unique operators are included. This approach will ensure that the optimal solutions achieved are accurate and reliable, while keeping the computational effort within acceptable limits also for an industrial application. The methodology implemented in OPTIMOrph will contribute to the inclusion of morphing technologies since the very early stages of the aircraft design process and will open unprecedented design opportunities to be applied either to re-engineering of current aircraft or to completely new upcoming aircraft architectures. Although very general, the procedure will be applied to a morphing wing leading edge, and a series of optimal indications will be delivered for implementing an integrated aerodynamic/structural proof of concept.

Deliverables

List of deliverables.
Publications and Information on Dissemination Activities	Documents, reports	2020-02-19 16:53:11
Dissemination and Exploitation Plan	Documents, reports	2020-02-19 16:53:10

Take a look to the deliverables list in detail: detailed list of OPTIMOrph deliverables.

Publications

List of publications.
year	authors and title	journal	last update
2019	Andrea Magrini, Ernesto Benini, Rita Ponza, Chen Wang, Hamed Khodaparast, Michael Friswell, Volker Landersheim, Dominik Laveuve, Conchin Contell Asins Comparison of Constrained Parameterisation Strategies for Aerodynamic Optimisation of Morphing Leading Edge Airfoil published pages: 31, ISSN: 2226-4310, DOI: 10.3390/aerospace6030031	Aerospace 6/3	2020-02-19
2019	C Wang, H Haddad Khodaparast, MI Friswell, A Magrini, R Ponza, E Benini, V Landersheim, D Laveuve, C Contell Asins Conceptual-level evaluation of a variable stiffness skin for a morphing wing leading edge published pages: 95441001985557, ISSN: 0954-4100, DOI: 10.1177/0954410019855576	Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering	2020-02-19

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The information about "OPTIMORPH" are provided by the European Opendata Portal: CORDIS opendata.