Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
26398 | 210 | 20.9 | 27% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
150 | 22256 | ENGINEERING FRACTURE MECHANICS//INTERNATIONAL JOURNAL OF FRACTURE//STRESS INTENSITY FACTOR |
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 | MULTIPLE SITE DAMAGE | Author keyword | 5 | 30% | 7% | 15 |
2 | MULTIPLE SITE DAMAGE MSD | Author keyword | 3 | 42% | 2% | 5 |
3 | STRIP YIELD MODEL | Author keyword | 2 | 22% | 5% | 10 |
4 | MODIFIED VIRTUAL CRACK CLOSURE INTEGRAL | Author keyword | 2 | 67% | 1% | 2 |
5 | THROUGH THE THICKNESS CRACK | Author keyword | 2 | 43% | 1% | 3 |
6 | GLASS FIBER REINFORCED LAMINATE GLARE | Author keyword | 1 | 100% | 1% | 2 |
7 | LIGAMENT FAILURE | Author keyword | 1 | 50% | 1% | 2 |
8 | MODE I TYPE DEFORMATION | Author keyword | 1 | 50% | 1% | 2 |
9 | MULTI SITE DAMAGE MSD | Author keyword | 1 | 100% | 1% | 2 |
10 | CIRCULAR ARC CRACK | Author keyword | 1 | 29% | 2% | 4 |
Web of Science journal categories |
Author Key Words |
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 | MULTIPLE SITE DAMAGE | 6 | 44% | 5% | 11 |
2 | AIRCRAFT FUSELAGE | 3 | 50% | 2% | 4 |
3 | CRACK GROWTH DATA | 2 | 67% | 1% | 2 |
4 | FUSELAGE STRUCTURES | 2 | 67% | 1% | 2 |
5 | SITE DAMAGE | 2 | 50% | 1% | 3 |
6 | ALTERNATING METHOD EPFEAM | 1 | 38% | 1% | 3 |
7 | WFD CONDITIONS | 1 | 38% | 1% | 3 |
8 | COLLINEAR UNEQUAL CRACKS | 1 | 100% | 1% | 2 |
9 | LINK UP | 1 | 100% | 1% | 2 |
10 | UNEQUAL CRACKS | 1 | 100% | 1% | 2 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
A COMPENDIUM OF SOURCES OF FRACTURE-TOUGHNESS AND FATIGUE CRACK-GROWTH DATA FOR METALLIC ALLOYS .3. | 1989 | 3 | 50 | 12% |
REFERENCES AND CONFERENCE PROCEEDINGS TOWARDS THE UNDERSTANDING OF FRACTURE-MECHANICS | 1986 | 0 | 17 | 47% |
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 | NAGOYA AEROSP SYST WORKS | 1 | 20% | 1.9% | 4 |
2 | DURABIL DAMAGE TOLERANCE BRANCH | 1 | 50% | 0.5% | 1 |
3 | FATIGUE DAMAGE TOLERANCE | 1 | 50% | 0.5% | 1 |
4 | UI CORP | 1 | 50% | 0.5% | 1 |
5 | WING DESIGN | 1 | 50% | 0.5% | 1 |
6 | MET FORMING TECHNOL SECT | 0 | 33% | 0.5% | 1 |
7 | STATE ENVIRONM SIMULAT | 0 | 13% | 0.5% | 1 |
8 | STRUCT ADV MAT | 0 | 13% | 0.5% | 1 |
9 | MECH MAT BRANCH | 0 | 11% | 0.5% | 1 |
10 | LRET EXCELLENCE | 0 | 10% | 0.5% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000208921 | T EPSILON INTEGRAL//CIRCULAR ARC CRACK//CRACK LINKUP |
2 | 0.0000150973 | FRACTAL FINITE ELEMENT METHOD//CONTACT CRACK PROBLEM//SHAPE SENSITIVITY ANALYSIS |
3 | 0.0000150098 | FATIGUE SENSOR//RANDOM FATIGUE CRACK GROWTH//SPATIAL RANDOM PROCESS |
4 | 0.0000140987 | COLD EXPANSION//FASTENER HOLES//RIVETED JOINTS |
5 | 0.0000130643 | CRACK SHAPE EVOLUTION//ROUND BAR//WEIGHT FUNCTION |
6 | 0.0000121631 | MODIFIED MAPPING COLLOCATION METHOD//PROPAGATING VELOCITY//LOW STRESS DROP |
7 | 0.0000116469 | ADHESIVE TENSILE STRENGTH//BROAD TRANSITION//HYCAR |
8 | 0.0000114865 | LIFE EXTENDING CONTROL//DAMAGE MITIGATING CONTROL//GUST LOAD ALLEVIATION SYSTEM |
9 | 0.0000114661 | CORROSION FATIGUE//PIT INDUCED CORROSION//CORROSION PIT |
10 | 0.0000110165 | T STRESS//ELASTIC T STRESS//WELD MISMATCH |