Water landings in emergency are likely to have tragic consequences for helicopters. Most of the safety devices developed to enhance helicopter crashworthiness have been designed referring to ground impacts and they might be not effective in case of water landings. At LAST, the crash labs of Politecnico di Milano, water impact drop tests were carried out to deepen the knowledge of the event dynamics and to collect reliable data to validate numerical models. The water impact behavior of skin panels made of aluminium alloy and carbon fiber reinforced plastic was investigated. Drop tests with several drop heights, different impacting masses and attitudes were performed measuring accelerations, deformations and pressures on the specimens. In the second part of the research, the tests were numerically reproduced adopting ALE and SPH approaches to model the fluid region. The numerical results were compared to the experimental tests in terms of impact dynamics and data acquired. As a result, a satisfactory correlation was achieved and guidelines to model fluid regions adopting ALE and SPH approaches were drawn.

Water Impact Drop Tests of Metallic and Composite Skin Panels and Numerical Simulations Using ALE and SPH Approaches

FRANCESCONI, EDOARDO;ANGHILERI, MARCO
2009-01-01

Abstract

Water landings in emergency are likely to have tragic consequences for helicopters. Most of the safety devices developed to enhance helicopter crashworthiness have been designed referring to ground impacts and they might be not effective in case of water landings. At LAST, the crash labs of Politecnico di Milano, water impact drop tests were carried out to deepen the knowledge of the event dynamics and to collect reliable data to validate numerical models. The water impact behavior of skin panels made of aluminium alloy and carbon fiber reinforced plastic was investigated. Drop tests with several drop heights, different impacting masses and attitudes were performed measuring accelerations, deformations and pressures on the specimens. In the second part of the research, the tests were numerically reproduced adopting ALE and SPH approaches to model the fluid region. The numerical results were compared to the experimental tests in terms of impact dynamics and data acquired. As a result, a satisfactory correlation was achieved and guidelines to model fluid regions adopting ALE and SPH approaches were drawn.
2009
65th American Helicopter Society International Annual Forum 2009
9781617829284
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/554193
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