Class information for: |
Basic class information |
| Class id | #P | Avg. number of references |
Database coverage of references |
|---|---|---|---|
| 30914 | 161 | 18.9 | 24% |
Hierarchy of classes |
The table includes all classes above and classes immediately below the current class. |
| Cluster id | Level | Cluster label | #P |
|---|---|---|---|
| 12 | 4 | POLYMER SCIENCE//MATERIALS SCIENCE, PAPER & WOOD//CHEMISTRY, PHYSICAL | 1084170 |
| 291 | 3 | JOURNAL OF CHEMICAL PHYSICS//CHEMISTRY, PHYSICAL//MOLECULAR PHYSICS | 41705 |
| 3431 | 2 | STOKES FLOW//SLIP FLOW SURFACE//BRINKMAN EQUATION | 1560 |
| 30914 | 1 | OSEEN FLOW//UER MATH PU PL//3D WAKES | 161 |
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 | OSEEN FLOW | authKW | 489118 | 4% | 37% | 7 |
| 2 | UER MATH PU PL | address | 252881 | 1% | 67% | 2 |
| 3 | 3D WAKES | authKW | 189662 | 1% | 100% | 1 |
| 4 | BIOMIMETIC SHIP PROPULSION | authKW | 189662 | 1% | 100% | 1 |
| 5 | EKMANS BOUNDARY LAYER | authKW | 189662 | 1% | 100% | 1 |
| 6 | ENERGY FROM WAVES | authKW | 189662 | 1% | 100% | 1 |
| 7 | EULERLETS | authKW | 189662 | 1% | 100% | 1 |
| 8 | HIGH ASPECT RATIO WING THEORY | authKW | 189662 | 1% | 100% | 1 |
| 9 | HYBRID PERTURBATION NUMERICAL METHOD | authKW | 189662 | 1% | 100% | 1 |
| 10 | IMPULSIVELY STARTED | authKW | 189662 | 1% | 100% | 1 |
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 | Mechanics | 1605 | 35% | 0% | 56 |
| 2 | Physics, Fluids & Plasmas | 904 | 19% | 0% | 30 |
| 3 | Mathematics, Applied | 801 | 29% | 0% | 46 |
| 4 | Mathematics, Interdisciplinary Applications | 325 | 11% | 0% | 17 |
| 5 | Multidisciplinary Sciences | 163 | 6% | 0% | 9 |
| 6 | Engineering, Ocean | 136 | 2% | 0% | 4 |
| 7 | Engineering, General | 136 | 7% | 0% | 12 |
| 8 | Engineering, Aerospace | 120 | 4% | 0% | 7 |
| 9 | Oceanography | 86 | 6% | 0% | 9 |
| 10 | Engineering, Mechanical | 82 | 8% | 0% | 13 |
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 | UER MATH PU PL | 252881 | 1% | 67% | 2 |
| 2 | ECOLE SUPER ENERGIE MAT | 131932 | 2% | 17% | 4 |
| 3 | AERODYNAM DESIGN DATA | 94830 | 1% | 50% | 1 |
| 4 | LCVMMSTN 8 | 94830 | 1% | 50% | 1 |
| 5 | MECAN ENERGET | 19570 | 2% | 3% | 4 |
| 6 | WATSON ENGN PL SCI | 9481 | 1% | 5% | 1 |
| 7 | LADHYX | 6004 | 2% | 1% | 3 |
| 8 | UMR CNRS 7554 | 3949 | 1% | 2% | 1 |
| 9 | LMM | 3887 | 1% | 1% | 2 |
| 10 | CFD TEAM | 3268 | 1% | 2% | 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 | SIAM JOURNAL ON APPLIED MATHEMATICS | 12375 | 9% | 0% | 15 |
| 2 | JOURNAL DE MECANIQUE THEORIQUE ET APPLIQUEE | 8589 | 2% | 1% | 4 |
| 3 | COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES SERIE B | 5534 | 1% | 1% | 2 |
| 4 | PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES | 3796 | 6% | 0% | 9 |
| 5 | COMPTES RENDUS DE L ACADEMIE DES SCIENCES SERIE II FASCICULE B-MECANIQUE PHYSIQUE CHIMIE ASTRONOMIE | 3541 | 1% | 1% | 2 |
| 6 | JOURNAL OF ENGINEERING MATHEMATICS | 2748 | 3% | 0% | 5 |
| 7 | COMPTES RENDUS DE L ACADEMIE DES SCIENCES SERIE II | 2036 | 6% | 0% | 9 |
| 8 | RECHERCHE AEROSPATIALE | 1961 | 1% | 1% | 2 |
| 9 | JSME INTERNATIONAL JOURNAL SERIES II-FLUIDS ENGINEERING HEAT TRANSFER POWER COMBUSTION THERMOPHYSICAL PROPERTIES | 1951 | 1% | 1% | 2 |
| 10 | ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK | 1841 | 3% | 0% | 5 |
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 | OSEEN FLOW | 489118 | 4% | 37% | 7 | Search OSEEN+FLOW | Search OSEEN+FLOW |
| 2 | 3D WAKES | 189662 | 1% | 100% | 1 | Search 3D+WAKES | Search 3D+WAKES |
| 3 | BIOMIMETIC SHIP PROPULSION | 189662 | 1% | 100% | 1 | Search BIOMIMETIC+SHIP+PROPULSION | Search BIOMIMETIC+SHIP+PROPULSION |
| 4 | EKMANS BOUNDARY LAYER | 189662 | 1% | 100% | 1 | Search EKMANS+BOUNDARY+LAYER | Search EKMANS+BOUNDARY+LAYER |
| 5 | ENERGY FROM WAVES | 189662 | 1% | 100% | 1 | Search ENERGY+FROM+WAVES | Search ENERGY+FROM+WAVES |
| 6 | EULERLETS | 189662 | 1% | 100% | 1 | Search EULERLETS | Search EULERLETS |
| 7 | HIGH ASPECT RATIO WING THEORY | 189662 | 1% | 100% | 1 | Search HIGH+ASPECT+RATIO+WING+THEORY | Search HIGH+ASPECT+RATIO+WING+THEORY |
| 8 | HYBRID PERTURBATION NUMERICAL METHOD | 189662 | 1% | 100% | 1 | Search HYBRID+PERTURBATION+NUMERICAL+METHOD | Search HYBRID+PERTURBATION+NUMERICAL+METHOD |
| 9 | IMPULSIVELY STARTED | 189662 | 1% | 100% | 1 | Search IMPULSIVELY+STARTED | Search IMPULSIVELY+STARTED |
| 10 | JET FLAPPED AEROFOIL | 189662 | 1% | 100% | 1 | Search JET+FLAPPED+AEROFOIL | Search JET+FLAPPED+AEROFOIL |
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 | CHADWICK, E , (2009) A SLENDER BODY THEORY IN OSEEN FLOW OBTAINED BY EXPANDING THE OSEENLETS IN THE GREEN'S INTEGRAL REPRESENTATION.FLUID DYNAMICS RESEARCH. VOL. 41. ISSUE 4. P. - | 7 | 78% | 1 |
| 2 | CHADWICK, E , KHAN, HM , MOATAMEDI, M , MAPPIN, M , PENNEY, M , (2010) EXPERIMENTAL VERIFICATION OF AN OSEEN FLOW SLENDER BODY THEORY.JOURNAL OF FLUID MECHANICS. VOL. 654. ISSUE . P. 271-279 | 5 | 100% | 1 |
| 3 | GEER, J , FILLO, J , (2008) FINITE DIFFERENCE SCHEMES FOR DIFFUSION PROBLEMS BASED ON A HYBRID PERTURBATION-GALERKIN METHOD.JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME. VOL. 130. ISSUE 6. P. - | 5 | 100% | 0 |
| 4 | SELLIER, A , (1999) ASYMPTOTIC SOLUTION FOR THE ELECTROSTATIC FIELD AROUND A SLENDER CONDUCTING BODY.IMA JOURNAL OF APPLIED MATHEMATICS. VOL. 62. ISSUE 2. P. 167-193 | 8 | 73% | 0 |
| 5 | CHADWICK, E , HATAM, A , (2009) A FURTHER NOTE ON THE FORCE DISCREPANCY FOR WING THEORY IN EULER FLOW.PROCEEDINGS OF THE INDIAN ACADEMY OF SCIENCES-MATHEMATICAL SCIENCES. VOL. 119. ISSUE 5. P. 679-698 | 5 | 83% | 0 |
| 6 | DEVINANT, P , GALLOIS, T , (2002) SWEPT AND CURVED WINGS: A NUMERICAL APPROACH BASED ON GENERALIZED LIFTING-LINE THEORY.COMPUTATIONAL MECHANICS. VOL. 29. ISSUE 4-5. P. 322-331 | 5 | 100% | 0 |
| 7 | SELLIER, A , (2001) A SLENDER DIELECTRIC BODY EMBEDDED IN AN ARBITRARY EXTERNAL POTENTIAL.IMA JOURNAL OF APPLIED MATHEMATICS. VOL. 66. ISSUE 2. P. 149-173 | 5 | 100% | 0 |
| 8 | CHADWICK, E , FISHWICK, N , (2007) LIFT ON SLENDER BODIES WITH ELLIPTICAL CROSS SECTION EVALUATED BY USING AN OSEEN FLOW MODEL.SIAM JOURNAL ON APPLIED MATHEMATICS. VOL. 67. ISSUE 5. P. 1465 -1478 | 4 | 100% | 6 |
| 9 | FISHWICK, N , CHADWICK, E , (2006) THE EVALUATION OF THE FAR-FIELD INTEGRAL IN THE GREEN'S FUNCTION REPRESENTATION FOR STEADY OSEEN FLOW.PHYSICS OF FLUIDS. VOL. 18. ISSUE 11. P. - | 4 | 100% | 3 |
| 10 | CHADWICK, E , RAHULAN, T , (2011) A THEORETICAL MODEL EVALUATING LEADING ORDER VORTEX DECAY BEHIND AN AIRCRAFT.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. VOL. 225. ISSUE G6. P. 657-663 | 8 | 42% | 1 |
Classes with closest relation at Level 1 |