Several experimental test cases are available in literature to study and validate fluid structure interaction methods. They, however, focus the attention mainly on replicating typical cruising aerodynamic conditions forcing the adoption of fully steel made models able to operate with the high loads generated in high speed facilities. This translates in a complete loss of similitude with typical realistic aeronautical wing structures configurations. To reverse this trend, and to better study the aerolastic mechanism from a structural point of view, an aeroelastic measurement campaign was carried within the EU RIBES project. A half wing model for wind tunnel tests was designed and manufactured replicating a typical metallic wing box structure, producing a database of loads, pressure, stress and deformation measurements. In this paper the design, manufacturing and validation activities performed within the RIBES project are described, with a focus on the structural behavior of the test article. All experimental data and numerical models are made freely available to the scientific community.

Structural validation of a realistic wing structure: the RIBES test article / Groth, C.; Porziani, S.; Chiappa, A.; Giorgetti, F.; Cella, U.; Nicolosi, F.; Della Vecchia, P.; Mastroddi, F.; Coppotelli, G.; Biancolin, i. M. E.. - In: PROCEDIA STRUCTURAL INTEGRITY. - ISSN 2452-3216. - 12:(2018), pp. 448-456. (Intervento presentato al convegno 47th International Conference on Stress Analysis, AIAS 2018 tenutosi a Villa San Giovanni; Italy) [10.1016/j.prostr.2018.11.073].

Structural validation of a realistic wing structure: the RIBES test article

Mastroddi F.;Coppotelli G.;
2018

Abstract

Several experimental test cases are available in literature to study and validate fluid structure interaction methods. They, however, focus the attention mainly on replicating typical cruising aerodynamic conditions forcing the adoption of fully steel made models able to operate with the high loads generated in high speed facilities. This translates in a complete loss of similitude with typical realistic aeronautical wing structures configurations. To reverse this trend, and to better study the aerolastic mechanism from a structural point of view, an aeroelastic measurement campaign was carried within the EU RIBES project. A half wing model for wind tunnel tests was designed and manufactured replicating a typical metallic wing box structure, producing a database of loads, pressure, stress and deformation measurements. In this paper the design, manufacturing and validation activities performed within the RIBES project are described, with a focus on the structural behavior of the test article. All experimental data and numerical models are made freely available to the scientific community.
2018
47th International Conference on Stress Analysis, AIAS 2018
FSI; experimental validation; dtructural validation; CFD; CSM
04 Pubblicazione in atti di convegno::04c Atto di convegno in rivista
Structural validation of a realistic wing structure: the RIBES test article / Groth, C.; Porziani, S.; Chiappa, A.; Giorgetti, F.; Cella, U.; Nicolosi, F.; Della Vecchia, P.; Mastroddi, F.; Coppotelli, G.; Biancolin, i. M. E.. - In: PROCEDIA STRUCTURAL INTEGRITY. - ISSN 2452-3216. - 12:(2018), pp. 448-456. (Intervento presentato al convegno 47th International Conference on Stress Analysis, AIAS 2018 tenutosi a Villa San Giovanni; Italy) [10.1016/j.prostr.2018.11.073].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1262267
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