Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
27011 | 240 | 21.7 | 26% |
Hierarchy of classes |
The table includes all classes above and classes immediately below the current class. |
Cluster id | Level | Cluster label | #P |
---|---|---|---|
16 | 4 | ENGINEERING, CIVIL//CONSTRUCTION & BUILDING TECHNOLOGY//MECHANICS | 627508 |
470 | 3 | INTERNATIONAL JOURNAL OF IMPACT ENGINEERING//ENERGY ABSORPTION//CRASHWORTHINESS | 24086 |
2944 | 2 | CRASHWORTHINESS//ENERGY ABSORPTION//AXIAL CRUSHING | 2693 |
27011 | 1 | SHIMMY//ADAPTIVE IMPACT ABSORPTION//FUSELAGE SECTION | 240 |
Terms with highest relevance score |
rank | Term | termType | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|---|
1 | SHIMMY | authKW | 855264 | 5% | 61% | 11 |
2 | ADAPTIVE IMPACT ABSORPTION | authKW | 763384 | 3% | 100% | 6 |
3 | FUSELAGE SECTION | authKW | 763384 | 3% | 100% | 6 |
4 | NOSE LANDING GEAR | authKW | 654327 | 3% | 86% | 6 |
5 | CRASHWORTHINESS IMPACTS STRUCT MECH GRP | address | 636153 | 2% | 100% | 5 |
6 | CONTROL LAW TEAM | address | 508922 | 2% | 100% | 4 |
7 | SHIMMY OSCILLATIONS | authKW | 508922 | 2% | 100% | 4 |
8 | LANDING GEAR | authKW | 461779 | 6% | 26% | 14 |
9 | SHIMMY VIBRATION | authKW | 407136 | 2% | 80% | 4 |
10 | AIRCRAFT CRASHWORTHINESS | authKW | 381692 | 1% | 100% | 3 |
Web of Science journal categories |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | Engineering, Aerospace | 16688 | 40% | 0% | 96 |
2 | Engineering, Mechanical | 4523 | 44% | 0% | 106 |
3 | Engineering, Manufacturing | 981 | 11% | 0% | 27 |
4 | Mechanics | 687 | 19% | 0% | 46 |
5 | Acoustics | 176 | 5% | 0% | 13 |
6 | Engineering, Biomedical | 108 | 6% | 0% | 14 |
7 | Instruments & Instrumentation | 97 | 7% | 0% | 17 |
8 | Engineering, Civil | 49 | 5% | 0% | 11 |
9 | Automation & Control Systems | 25 | 3% | 0% | 6 |
10 | Engineering, Ocean | 20 | 1% | 0% | 2 |
Address terms |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | CRASHWORTHINESS IMPACTS STRUCT MECH GRP | 636153 | 2% | 100% | 5 |
2 | CONTROL LAW TEAM | 508922 | 2% | 100% | 4 |
3 | LANDING GEAR SYST | 381692 | 1% | 100% | 3 |
4 | INTEGRATED FLIGHT CONTROL SYST DIRECTORATE | 339279 | 2% | 67% | 4 |
5 | FUNDAMENTAL SCI DEF ADV DESIGN TECHN | 318062 | 4% | 25% | 10 |
6 | CIVIL AIRCRAFT AIRWORTHINESS CERTIFICAT TECHNOL | 254461 | 1% | 100% | 2 |
7 | AIRCRAFT STRUCT GRP | 127231 | 0% | 100% | 1 |
8 | BAUWEISEN KONSTRUKTIONSFOR | 127231 | 0% | 100% | 1 |
9 | CRASHWORTHINESS | 127231 | 0% | 100% | 1 |
10 | CRASHWORTHINESS IMPACT STRUCT MECH GRP CISM | 127231 | 0% | 100% | 1 |
Journals |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | INTERNATIONAL JOURNAL OF CRASHWORTHINESS | 105740 | 11% | 3% | 26 |
2 | JOURNAL OF AIRCRAFT | 36844 | 17% | 1% | 41 |
3 | JOURNAL OF THE AMERICAN HELICOPTER SOCIETY | 33889 | 6% | 2% | 15 |
4 | AEROSPACE ENGINEERING | 18172 | 1% | 7% | 2 |
5 | VEHICLE SYSTEM DYNAMICS | 12865 | 6% | 1% | 15 |
6 | JOURNAL OF VIBROENGINEERING | 11121 | 5% | 1% | 13 |
7 | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 4811 | 3% | 0% | 8 |
8 | CHINESE JOURNAL OF AERONAUTICS | 2543 | 2% | 0% | 5 |
9 | AEROSPACE SCIENCE AND TECHNOLOGY | 2198 | 3% | 0% | 6 |
10 | JOURNAL OF AEROSPACE ENGINEERING | 2046 | 2% | 0% | 4 |
Author Key Words |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
LCSH search | Wikipedia search |
---|---|---|---|---|---|---|---|
1 | SHIMMY | 855264 | 5% | 61% | 11 | Search SHIMMY | Search SHIMMY |
2 | ADAPTIVE IMPACT ABSORPTION | 763384 | 3% | 100% | 6 | Search ADAPTIVE+IMPACT+ABSORPTION | Search ADAPTIVE+IMPACT+ABSORPTION |
3 | FUSELAGE SECTION | 763384 | 3% | 100% | 6 | Search FUSELAGE+SECTION | Search FUSELAGE+SECTION |
4 | NOSE LANDING GEAR | 654327 | 3% | 86% | 6 | Search NOSE+LANDING+GEAR | Search NOSE+LANDING+GEAR |
5 | SHIMMY OSCILLATIONS | 508922 | 2% | 100% | 4 | Search SHIMMY+OSCILLATIONS | Search SHIMMY+OSCILLATIONS |
6 | LANDING GEAR | 461779 | 6% | 26% | 14 | Search LANDING+GEAR | Search LANDING+GEAR |
7 | SHIMMY VIBRATION | 407136 | 2% | 80% | 4 | Search SHIMMY+VIBRATION | Search SHIMMY+VIBRATION |
8 | AIRCRAFT CRASHWORTHINESS | 381692 | 1% | 100% | 3 | Search AIRCRAFT+CRASHWORTHINESS | Search AIRCRAFT+CRASHWORTHINESS |
9 | LMS SIMULATION | 381692 | 1% | 100% | 3 | Search LMS+SIMULATION | Search LMS+SIMULATION |
10 | VEHICLE SHIMMY | 381692 | 1% | 100% | 3 | Search VEHICLE+SHIMMY | Search VEHICLE+SHIMMY |
Core articles |
The table includes core articles in the class. The following variables is taken into account for the relevance score of an article in a cluster c: (1) Number of references referring to publications in the class. (2) Share of total number of active references referring to publications in the class. (3) Age of the article. New articles get higher score than old articles. (4) Citation rate, normalized to year. |
Rank | Reference | # ref. in cl. |
Shr. of ref. in cl. |
Citations |
---|---|---|---|---|
1 | YU, ZF , GU, HS , WANG, H , YI, PY , (2013) CRASH SIMULATION OF THE FUSELAGE SECTION WITH CENTRAL WING BOX FOR A REGIONAL JET.INTERNATIONAL JOURNAL OF CRASHWORTHINESS. VOL. 18. ISSUE 1. P. 19-28 | 15 | 88% | 0 |
2 | REN, Y , XIANG, J , (2014) ENERGY ABSORPTION STRUCTURES DESIGN OF CIVIL AIRCRAFT TO IMPROVE CRASHWORTHINESS.AERONAUTICAL JOURNAL. VOL. 118. ISSUE 1202. P. 383 -398 | 11 | 92% | 1 |
3 | ARREAZA, C , BEHDINAN, K , ZU, JW , (2016) LINEAR STABILITY ANALYSIS AND DYNAMIC RESPONSE OF SHIMMY DAMPERS FOR MAIN LANDING GEARS.JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME. VOL. 83. ISSUE 8. P. - | 9 | 100% | 0 |
4 | RAN, SH , BESSELINK, IJM , NIJMEIJER, H , (2014) APPLICATION OF NONLINEAR TYRE MODELS TO ANALYSE SHIMMY.VEHICLE SYSTEM DYNAMICS. VOL. 52. ISSUE . P. 387-404 | 8 | 100% | 0 |
5 | REN, YR , XIANG, JW , ZHENG, JQ , LUO, ZP , (2016) CRASHWORTHINESS ANALYSIS OF AIRCRAFT FUSELAGE WITH SINE-WAVE BEAM STRUCTURE.CHINESE JOURNAL OF AERONAUTICS. VOL. 29. ISSUE 2. P. 403 -410 | 9 | 82% | 0 |
6 | SBARUFATTI, C , VALLONE, G , GIGLIO, M , STEFANIUK, M , LESKI, A , ZIELINSKI, W , (2016) EXPERIMENTAL VALIDATION OF A COMPUTATIONAL HYBRID METHODOLOGY TO ESTIMATE FUSELAGE DAMAGE DUE TO HARSH LANDING.JOURNAL OF THE AMERICAN HELICOPTER SOCIETY. VOL. 61. ISSUE 4. P. - | 10 | 71% | 0 |
7 | FENG, F , NIE, H , ZHANG, M , PENG, YM , (2015) EFFECT OF TORSIONAL DAMPING ON AIRCRAFT NOSE LANDING-GEAR SHIMMY.JOURNAL OF AIRCRAFT. VOL. 52. ISSUE 2. P. 561 -568 | 10 | 71% | 0 |
8 | ORLANDO, C , ALAIMO, A , (2017) A ROBUST ACTIVE CONTROL SYSTEM FOR SHIMMY DAMPING IN THE PRESENCE OF FREE PLAY AND UNCERTAINTIES.MECHANICAL SYSTEMS AND SIGNAL PROCESSING. VOL. 84. ISSUE . P. 551 -569 | 13 | 52% | 0 |
9 | HOWCROFT, C , LOWENBERG, M , NEILD, S , KRAUSKOPF, B , COETZEE, E , (2015) SHIMMY OF AN AIRCRAFT MAIN LANDING GEAR WITH GEOMETRIC COUPLING AND MECHANICAL FREEPLAY.JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS. VOL. 10. ISSUE 5. P. - | 9 | 69% | 1 |
10 | ZHENG, JQ , XIANG, JW , LUO, ZP , REN, YR , (2011) CRASHWORTHINESS DESIGN OF TRANSPORT AIRCRAFT SUBFLOOR USING POLYMER FOAMS.INTERNATIONAL JOURNAL OF CRASHWORTHINESS. VOL. 16. ISSUE 4. P. 375 -383 | 9 | 75% | 8 |
Classes with closest relation at Level 1 |