A multidisciplinary approach is implemented to model and analyze the performance of Olympic rowing boats. A reduced-order model that couples rowers motions with the hull, oars and hydrodynamic and hydrostatic forces is detailed. This model is complemented with a sensitivity analysis carried out by means of a non intrusive polynomial chaos expansion. Different strategies for the evaluation of the polynomial chaos expansion coefficients are implemented and tested. Sensitivity analysis results for a lightweight single scull are presented and discussed. This analysis contrasts the effects of varying forces exerted by the rowers, weights of rowers and cadence of motions on the boat performance. © 2010 by A. Mola, M. Ghommem and M. R. Hajj.

Sensitivity analysis of the performance of olympic rowing boats / Mola, A.; Ghommem, M.; Hajj, M. R.. - (2010), pp. 1-10. (Intervento presentato al convegno 13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, MAO 2010 tenutosi a Ft. Worth, TX, usa nel 13 September 2010 through 15 September 2010) [10.2514/6.2010-9395].

Sensitivity analysis of the performance of olympic rowing boats

Mola A.;
2010-01-01

Abstract

A multidisciplinary approach is implemented to model and analyze the performance of Olympic rowing boats. A reduced-order model that couples rowers motions with the hull, oars and hydrodynamic and hydrostatic forces is detailed. This model is complemented with a sensitivity analysis carried out by means of a non intrusive polynomial chaos expansion. Different strategies for the evaluation of the polynomial chaos expansion coefficients are implemented and tested. Sensitivity analysis results for a lightweight single scull are presented and discussed. This analysis contrasts the effects of varying forces exerted by the rowers, weights of rowers and cadence of motions on the boat performance. © 2010 by A. Mola, M. Ghommem and M. R. Hajj.
2010
13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 2010
1
10
978-1-60086-954-9
https://arc.aiaa.org/doi/10.2514/6.2010-9395
American Institute of Aeronautics and Astronautics
Mola, A.; Ghommem, M.; Hajj, M. R.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.11767/115052
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