2019
DOI: 10.1007/s00158-018-2143-8
|View full text |Cite
|
Sign up to set email alerts
|

Topology optimization of multi-directional variable thickness thin plate with multiple materials

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
4
1

Citation Types

1
7
0

Year Published

2019
2019
2024
2024

Publication Types

Select...
9

Relationship

0
9

Authors

Journals

citations
Cited by 35 publications
(8 citation statements)
references
References 25 publications
1
7
0
Order By: Relevance
“…Substituting Eqs. (13), (19), (26) and (27) into Eq. (11) and using following relation for conical shells:…”
Section: Governing Equationsmentioning
confidence: 99%
See 1 more Smart Citation
“…Substituting Eqs. (13), (19), (26) and (27) into Eq. (11) and using following relation for conical shells:…”
Section: Governing Equationsmentioning
confidence: 99%
“…Reduction in weight and increase in strength and stiffness of structures is one of the most important challenges for mechanical engineers which has been solved in the recent years using multi-phase materials [17][18][19] and different types of nanoreinforcements such as single-walled carbon nanotubes (SWC-NTs), multi-walled carbon nanotubes (MWCNTs) and GNPs. In comparison with SWCNTs and MWCNTs, GNPs have bigger specific surface area which creates stronger bonding with the matrix and significantly enhanced load transfer capability [20].…”
Section: Introductionmentioning
confidence: 99%
“…Lambe et al 6 proposed a topology optimization method combining continuous material field with adaptive mesh refinement, which used different design and analysis grids to avoid islands of materials in the topology configuration, and adopted Helmholtz-type density filter to avoid some unnecessary small features in the design and analysis of mesh refinement. Banh et al 7 , 8 used topology optimization method to study multiphase material and multiple materials plate structure problem, and then they presented an effective non-homogeneous multi-material topology optimization paradigm for functionally graded structures considering both cracked and non‐cracked cases 9 .…”
Section: Introductionmentioning
confidence: 99%
“…One attractive problem in the field of aerospace is the optimization of the blade structure through the improvement of the stiffness and stiffness to mass ratio utilizing the variable thickness technique. 18,[25][26][27][28] Figure 1 shows a schematic description of a rotary blade with the main load-carrying interior variable thickness spar box beam structure. The latter is composed of FGMs which are potentially suitable candidates for aeronautical structures.…”
Section: Introductionmentioning
confidence: 99%