Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
7366 | 1297 | 21.7 | 44% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
143 | 22311 | MATERIALS SCIENCE, COMPOSITES//JOURNAL OF COMPOSITE MATERIALS//COMPOSITE STRUCTURES |
Terms with highest relevance score |
Rank | Term | Type of term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|---|
1 | LAMINATION PARAMETERS | Author keyword | 54 | 83% | 2% | 30 |
2 | POLAR METHOD | Author keyword | 41 | 81% | 2% | 25 |
3 | VARIABLE STIFFNESS PANELS | Author keyword | 21 | 90% | 1% | 9 |
4 | FIBRE STEERING | Author keyword | 15 | 88% | 1% | 7 |
5 | ADV MAT DESIGN MANU TURE | Address | 11 | 100% | 0% | 6 |
6 | COMPOSITE STIFFENED PANELS | Author keyword | 11 | 69% | 1% | 9 |
7 | CUTOUTS | Author keyword | 10 | 54% | 1% | 13 |
8 | POSTBUCKLING | Author keyword | 8 | 14% | 4% | 55 |
9 | LAMINATION PARAMETER | Author keyword | 8 | 75% | 0% | 6 |
10 | FIBER STEERING | Author keyword | 8 | 100% | 0% | 5 |
Web of Science journal categories |
Author Key Words |
Rank | Web of Science journal category | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
LCSH search | Wikipedia search |
---|---|---|---|---|---|---|---|
1 | LAMINATION PARAMETERS | 54 | 83% | 2% | 30 | Search LAMINATION+PARAMETERS | Search LAMINATION+PARAMETERS |
2 | POLAR METHOD | 41 | 81% | 2% | 25 | Search POLAR+METHOD | Search POLAR+METHOD |
3 | VARIABLE STIFFNESS PANELS | 21 | 90% | 1% | 9 | Search VARIABLE+STIFFNESS+PANELS | Search VARIABLE+STIFFNESS+PANELS |
4 | FIBRE STEERING | 15 | 88% | 1% | 7 | Search FIBRE+STEERING | Search FIBRE+STEERING |
5 | COMPOSITE STIFFENED PANELS | 11 | 69% | 1% | 9 | Search COMPOSITE+STIFFENED+PANELS | Search COMPOSITE+STIFFENED+PANELS |
6 | CUTOUTS | 10 | 54% | 1% | 13 | Search CUTOUTS | Search CUTOUTS |
7 | POSTBUCKLING | 8 | 14% | 4% | 55 | Search POSTBUCKLING | Search POSTBUCKLING |
8 | LAMINATION PARAMETER | 8 | 75% | 0% | 6 | Search LAMINATION+PARAMETER | Search LAMINATION+PARAMETER |
9 | FIBER STEERING | 8 | 100% | 0% | 5 | Search FIBER+STEERING | Search FIBER+STEERING |
10 | VARIABLE STIFFNESS COMPOSITES | 8 | 100% | 0% | 5 | Search VARIABLE+STIFFNESS+COMPOSITES | Search VARIABLE+STIFFNESS+COMPOSITES |
Key Words Plus |
Rank | Web of Science journal category | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | STACKING SEQUENCE OPTIMIZATION | 50 | 77% | 3% | 34 |
2 | MAXIMUM BUCKLING LOAD | 38 | 93% | 1% | 14 |
3 | LAMINATION PARAMETERS | 27 | 78% | 1% | 18 |
4 | BUCKLING LOAD MAXIMIZATION | 20 | 100% | 1% | 9 |
5 | STACKING SEQUENCE | 20 | 35% | 3% | 45 |
6 | POLAR METHOD | 18 | 83% | 1% | 10 |
7 | LAYERWISE OPTIMIZATION | 17 | 79% | 1% | 11 |
8 | BUCKLING LOAD | 16 | 56% | 1% | 19 |
9 | STIFFENED PANELS | 15 | 40% | 2% | 29 |
10 | PANDA2 | 15 | 88% | 1% | 7 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Optimum stacking sequence design of composite materials Part II: Variable stiffness design | 2010 | 46 | 82 | 70% |
Optimum stacking sequence design of composite materials Part I: Constant stiffness design | 2009 | 50 | 97 | 72% |
A review of optimization techniques used in the design of fibre composite structures for civil engineering applications | 2012 | 20 | 48 | 35% |
A review on the mechanical behaviour of curvilinear fibre composite laminated panels | 2014 | 1 | 86 | 70% |
Buckling Analysis of Variable Angle Tow Composite Plates Using Differential Quadrature Method | 2013 | 1 | 11 | 82% |
Modelling the effect of gaps and overlaps in automated fibre placement (AFP)-manufactured laminates | 2015 | 0 | 12 | 50% |
Structural Health Monitoring of Composite Aircraft Structures Using Fiber Bragg Grating Sensors | 2013 | 2 | 8 | 25% |
Optimal Design of Composite Structures: A Historical Review | 2013 | 0 | 66 | 38% |
COMPUTER-PROGRAMS FOR MECHANICAL ANALYSIS AND DESIGN OF POLYMER MATRIX COMPOSITES | 1994 | 2 | 32 | 56% |
Address terms |
Rank | Address term | Relevance score (tfidf) |
Class's shr. of term's tot. occurrences |
Shr. of publ. in class containing term |
Num. of publ. in class |
---|---|---|---|---|---|
1 | ADV MAT DESIGN MANU TURE | 11 | 100% | 0.5% | 6 |
2 | AEROSP STRUCT CHAIR | 4 | 56% | 0.4% | 5 |
3 | CADENCE | 3 | 50% | 0.4% | 5 |
4 | ADV MAT DESIGN PROTOTYPING | 3 | 100% | 0.2% | 3 |
5 | DEMEC INEGI | 3 | 100% | 0.2% | 3 |
6 | ADV MAT DESIGN MFG | 3 | 45% | 0.4% | 5 |
7 | COMPOSITE STRUCT DEV | 3 | 60% | 0.2% | 3 |
8 | AD TRON FUNKT INTEGRAT | 2 | 67% | 0.2% | 2 |
9 | FOMAAS | 2 | 67% | 0.2% | 2 |
10 | COMPOSITE STRUCTU AD T SYST | 2 | 50% | 0.2% | 3 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000189562 | PRE COMPRESSION RINGS//2 D RANDOM FIELDS//FRANGIBLE COVER |
2 | 0.0000149514 | COMPOSITE T JOINT//SANDWICH T JOINT//TRANSVERSE STITCHING |
3 | 0.0000127828 | SHELL BUCKLING//KNOCK DOWN FACTOR//PFH |
4 | 0.0000101115 | RANDOM SYSTEM PROPERTIES//AERONAUT AEROSP ENGN//GENERALIZED UNIFIED FORMULATION |
5 | 0.0000097906 | C 1 HOMOTOPY//VIBRATIONAL ISOTOPE EFFECT//INTERACTION OF QUANTUM SYSTEMS |
6 | 0.0000095921 | BOLTED JOINTS//PINNED JOINT//BEARING STRENGTH |
7 | 0.0000093816 | DYNAMIC BUCKLING//STRENGTH MAT STRUCT K12//TEACHING SECT MAT MECH |
8 | 0.0000090643 | PLATES WITH CUTOUTS//36NI FE ALLOY//KNITTING ZONE |
9 | 0.0000090296 | INTERLAMINAR STRESSES//FREE EDGE EFFECT//FREE CORNER EFFECT |
10 | 0.0000083237 | FILAMENT WINDING//ROBOTIZED FILAMENT WINDING//REINFORCED THERMOPLASTIC PIPE |