2014
DOI: 10.1007/s00419-014-0929-8
|View full text |Cite
|
Sign up to set email alerts
|

A shear deformable cylindrical shell model based on couple stress theory

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
19
0

Year Published

2016
2016
2022
2022

Publication Types

Select...
9
1

Relationship

0
10

Authors

Journals

citations
Cited by 63 publications
(19 citation statements)
references
References 21 publications
0
19
0
Order By: Relevance
“…In contrast to the classical theory which is not able to justify the mechanical response of the micro-scale structures, non-classical theories, such as couple stress theory [14][15][16] and modi ed couple stress theory [17][18][19], are appropriately able to explain this phenomenon and cover the gap between the experimental and classical theory results. Couple stress theory as a theory is capable of explaining the size-dependent behavior of mechanisms proposed for the rst time by Mindlin and Tiersten [14].…”
Section: Introductionmentioning
confidence: 93%
“…In contrast to the classical theory which is not able to justify the mechanical response of the micro-scale structures, non-classical theories, such as couple stress theory [14][15][16] and modi ed couple stress theory [17][18][19], are appropriately able to explain this phenomenon and cover the gap between the experimental and classical theory results. Couple stress theory as a theory is capable of explaining the size-dependent behavior of mechanisms proposed for the rst time by Mindlin and Tiersten [14].…”
Section: Introductionmentioning
confidence: 93%
“…The micro-plates and micro-beams have found to be extensively applied in nano-/micro-electrical mechanical systems (NEMS/MEMS). The size-dependent behavior of these microscale structures also has been indicated in many experiments [10]. This phenomenon was first realized in much plastic deformation in metals and polymers.…”
Section: Introductionmentioning
confidence: 68%
“…Based on the Navier solution method and according to FSDT cylindrical shell model, for simply supported ends, the MT displacement field solutions are considered as follows: 32,62 u = U cos mπ L x cos (nθ) e iωt ;…”
Section: Solving Methodsmentioning
confidence: 99%