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Analytical similitudes applied to thin cylindrical shells

De Rosa, Sergio, Franco, Francesco·2015·Advances in aircraft and spacecraft science

Abstract

This work is focused on the definition and the analysis of both complete and incomplete similitudes for the dynamic responses of thin shells. Previous numerical and experimental investigations on both structural and structural-acoustic systems motivated this further analysis, mainly centred on the incomplete (distorted) similitudes. These similitudes and the associated scaling laws are defined by using the classical modal approach (CMA) and by invoking also the Energy Distribution Approach (EDA) in order to take into account both the cinematic and energetic items. The whole procedure is named SAMSARA: Similitude and Asymptotic Models for Structural-Acoustic Research and Applications. A brief summary of the procedure is herein given and the attention is paid to the analytical models of thin stiffened and unstiffened cylindrical shells. By using the well-known smeared model, the stiffened cylinder equations are used as general framework to analyse the possibility to define exact (replicas) or distorted similitudes (avatars). Despite the extreme simplicity of the proposed models, the results are really encouraging. The final aim is to define equivalent models to be used in laboratory measurements.

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Crossref · 10.12989/aas.2015.2.4.403

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  • Systems with the same dimensionless parameter groups tend to behave in a similar manner and respond similarly to perturbations.

    “In engineering this principle is called similitude analysis54,55, where systems with the same dimensionless parameter groups tend to behave in a similar manner and respond similarly to perturbations.”

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Research works printed but not linked: 12

  1. 2015, Mech. Syst. Signal Pr., 52-53, 722, 10.1016/j.ymssp.2014.06.007 · DOI
  2. 2011, Mech. Syst. Signal Pr., 25, 969, 10.1016/j.ymssp.2010.10.004 · DOI
  3. 2012, Mech. Syst. Signal Pr., 30, 330, 10.1016/j.ymssp.2012.01.018 · DOI
  4. 2004, Compos. Part B, 35, 599, 10.1016/j.compositesb.2003.11.003 · DOI
  5. 1989, Brit. J. Phil. Scie., 40, 145, 10.1093/bjps/40.2.145 · DOI
  6. 2003, J. Sound Vib., 264, 391, 10.1016/S0022-460X(02)01201-4 · DOI
  7. 1996, J. Sound Vib., 195, 301, 10.1006/jsvi.1996.0423 · DOI
  8. 2008, Key Eng. Mater., 385-387, 609, 10.4028/www.scientific.net/KEM.385-387.609 · DOI
  9. 2008, J. Sound Vib., 311, 314, 10.1016/j.jsv.2007.09.006 · DOI
  10. 2009, Thin Wall. Struct.,, 47, 1316, 10.1016/j.tws.2009.03.013 · DOI
  11. 2006, Comput. Struct., 84, 102, 10.1016/j.compstruc.2005.09.033 · DOI
  12. 2010, Key Eng. Mater., 417, 742

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Metadata

Authors
De Rosa, S., & Franco, F.
Venue
Advances in aircraft and spacecraft science
Publisher
Techno-Press
Published
2015-10-25
Volume
2
Issue
4
Pages
403-425
ISSN
2287-528X
Cited by
12
References
0
Language
en

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