Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Suganyadevi Sarangan"'
Autor:
Suganyadevi Sarangan, Singh, B.N.
Publikováno v:
In Aerospace Science and Technology May 2016 52:243-255
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science. 236:397-411
In this present work, non-polynomial zigzag theories (algebraic zigzag theory (AZT), exponential zigzag theory (EZT), hyperbolic zigzag theory (HZT), inverse hyperbolic zigzag theory (IZT), logarithmic zigzag theory (LZT) and trigonometric zigzag the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b93556ad221b32ec9c081d096a5bf7a8
https://doi.org/10.1177/09544062211020044
https://doi.org/10.1177/09544062211020044
Publikováno v:
Mechanics of Advanced Materials and Structures. 29:5608-5623
In the present work, nonlinear free vibration analysis of composite laminated plates and shallow cylindrical/spherical/hyperboloid shell panels considering geometric nonlinearity is carried out usi...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87b929181c21ff8a22002ac074f87b6d
https://doi.org/10.1080/15376494.2021.1959971
https://doi.org/10.1080/15376494.2021.1959971
Publikováno v:
Composite Structures. 206:967-977
In the present study, epistemic uncertainty is quantified for bending and buckling analysis of laminated composite plates using evidence theory. By employing vertex and uniform sampling methods the degree of confidence of the failure analysis is carr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b78d1806fc5bf6ad3bf166d8c411b1cb
https://doi.org/10.1016/j.compstruct.2018.07.097
https://doi.org/10.1016/j.compstruct.2018.07.097
Publikováno v:
Aerospace Science and Technology. 68:496-508
The present work deals with prediction of bending and free vibration analysis of laminated composite and sandwich plates using non-polynomial zigzag theories inline with C 0 finite element formulation. The assumed mathematical model is the combinatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::089582dde8e7d7c9c10d36dd02514880
https://doi.org/10.1016/j.ast.2017.06.001
https://doi.org/10.1016/j.ast.2017.06.001
Publikováno v:
Aerospace Science and Technology. 52:243-255
In this present work, improved zigzag theories are developed for the flexural analysis of laminated plates using algebraic, hyperbolic, inverse trigonometric and trigonometric shear strain functions. The governing differential equations and boundary
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5c6731f676d23e83d72325a30f30045e
https://doi.org/10.1016/j.ast.2016.02.034
https://doi.org/10.1016/j.ast.2016.02.034
Publikováno v:
Composite Structures. 138:391-403
In the present study, new shear deformation theories (algebraic (ADT), exponential (EDT), hyperbolic (HDT), logarithmic (LDT) and trigonometric (TDT)) were developed to analyze the static, buckling and free vibration responses of laminated composite
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fbf92cb7066a23069f1baa058688f0d7
https://doi.org/10.1016/j.compstruct.2015.11.049
https://doi.org/10.1016/j.compstruct.2015.11.049