Zobrazeno 1 - 10
of 46
pro vyhledávání: '"Zhanming Qin"'
Calculation of the added mass matrix of water impact of elastic wedges by the discrete vortex method
Autor:
Xiaowu Fu, Zhanming Qin
Publikováno v:
Journal of Fluids and Structures. 44:316-323
The discrete vortex method is used to obtain the added mass matrix of water entry of elastic structures. Based on the Wagner theory, the hydrodynamic loads are evaluated by the “flat-disc” approximation. The structural deformation is described by
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dde232d02d2ec297b443ea21f275ce0b
https://doi.org/10.1016/j.jfluidstructs.2013.11.008
https://doi.org/10.1016/j.jfluidstructs.2013.11.008
Publikováno v:
Thin-Walled Structures. 73:242-251
Modal interactions of a geometrically nonlinear sandwich beam with transversely compressible core in the presence of combination internal resonance are investigated. At first, a geometrically nonlinear, {2,1}-order theory is used to derived the equat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87b8f9aebedf98d10f544099687cbb19
https://doi.org/10.1016/j.tws.2013.07.014
https://doi.org/10.1016/j.tws.2013.07.014
Publikováno v:
Aerospace Science and Technology. 25:242-252
This paper addresses the robust aeroelastic instability suppression of an advanced aircraft wing modeled as a thin-walled beam structure with fiber-reinforced composite material featuring a circumferentially asymmetric stiffness (CAS) configuration.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7be313940783cc33ff9a27d1ddcad96
https://doi.org/10.1016/j.ast.2012.01.012
https://doi.org/10.1016/j.ast.2012.01.012
Publikováno v:
Journal of Aerospace Engineering. 25:320-333
The robust vibration control and dynamic response analysis of an advanced aircraft wing structure are addressed in this paper. The wing structure is modeled as a thin-walled beam with fiber-reinforced composite materials featuring a circumferentially
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::42e42f74797759fbe373261c95b3c2b3
https://doi.org/10.1061/(asce)as.1943-5525.0000121
https://doi.org/10.1061/(asce)as.1943-5525.0000121
Publikováno v:
Journal of Sound and Vibration. 330:4998-5013
The dynamic aeroelastic response and its active control of composite beam structures in compressible flow and exposed to gust and explosive type loads are examined. Modeling of the structures is based on a refined composite thin-walled beam theory an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cb7816f7ad2ee87b026b356ab198ccb
https://doi.org/10.1016/j.jsv.2011.05.026
https://doi.org/10.1016/j.jsv.2011.05.026
Autor:
Zhanming Qin, Davresh Hasanyan
Publikováno v:
International Journal of Non-Linear Mechanics. 46:425-435
By using the mixed Lagrangian–Eulerian description and adopting the von Karman's strain approximation, the non-linear magnetoelastic interactions of a circular cylindrical thin shell experiencing moderately large deflections are fully explored. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1658c0689058642a616d5d5fc0142cee
https://doi.org/10.1016/j.ijnonlinmec.2010.11.002
https://doi.org/10.1016/j.ijnonlinmec.2010.11.002
Autor:
Zhanming Qin
Publikováno v:
International Journal of Engineering Science. 48:1797-1810
The magneto-thermo-elastic interactions of a circular cylindrical shell immersed in applied magnetic and thermal fields are modeled and the shell’ nonlinear response and stability are investigated. The shell is made of a transversely isotropic, per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c709aba248ce7ec2d5aca4d58125e936
https://doi.org/10.1016/j.ijengsci.2010.09.021
https://doi.org/10.1016/j.ijengsci.2010.09.021
Publikováno v:
International Journal of Applied Electromagnetics and Mechanics. 31:79-96
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57959d029c2b2a2b695520172083e0bd
https://doi.org/10.3233/jae-2009-1049
https://doi.org/10.3233/jae-2009-1049
Publikováno v:
Journal of Sound and Vibration. 318:74-92
In this paper, the dynamic aeroelastic response and the related robust control of aircraft swept wings exposed to gust and explosive type loads are examined. The structural model of the wing is in the form of a thin/thick-walled beam and incorporates
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::465553c631bce1583e802cd3dd00225d
https://doi.org/10.1016/j.jsv.2008.04.007
https://doi.org/10.1016/j.jsv.2008.04.007
Autor:
Xiao Wang, Zhanming Qin
Nonlinear dynamic characteristics of a composite aircraft wing structure modeled by a geometrically nonlinear anisotropic thin-walled beam in the presence of simultaneous 1:2 internal and 1:1 external resonances are investigated. Some prominent non-c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::41f0bbfdac8b1aa6de110c7a43f51b57
http://hdl.handle.net/11311/1026420
http://hdl.handle.net/11311/1026420
