Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 33520 | 90 | 20.5 | 18% |
Classes in level above (level 2) |
| ID, lev. above |
Publications | Label for level above |
|---|---|---|
| 429 | 15725 | JOURNAL OF COMPUTATIONAL PHYSICS//INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS//COMPUTERS & FLUIDS |
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 | CUBIC BOUNDARY ELEMENT | Author keyword | 1 | 100% | 2% | 2 |
| 2 | BALANCE RELATIONS | Author keyword | 1 | 50% | 1% | 1 |
| 3 | DIPARTIMENTO METODI MODELLI MATEMAT SCI PLIC | Address | 1 | 50% | 1% | 1 |
| 4 | HEXAHEDRAL GRIDS | Author keyword | 1 | 50% | 1% | 1 |
| 5 | POWER UNIT | Address | 1 | 50% | 1% | 1 |
| 6 | SINGULAR BOUNDARY INTEGRAL EQUATION | Author keyword | 1 | 29% | 2% | 2 |
| 7 | EADS MIL AIRCRAFT | Address | 0 | 33% | 1% | 1 |
| 8 | EFFECT OF VISCOSITY | Author keyword | 0 | 33% | 1% | 1 |
| 9 | HIGH ORDER BEM | Author keyword | 0 | 33% | 1% | 1 |
| 10 | MODIFIED SHAPE FUNCTIONS | Author keyword | 0 | 33% | 1% | 1 |
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 | CUBIC BOUNDARY ELEMENT | 1 | 100% | 2% | 2 | Search CUBIC+BOUNDARY+ELEMENT | Search CUBIC+BOUNDARY+ELEMENT |
| 2 | BALANCE RELATIONS | 1 | 50% | 1% | 1 | Search BALANCE+RELATIONS | Search BALANCE+RELATIONS |
| 3 | HEXAHEDRAL GRIDS | 1 | 50% | 1% | 1 | Search HEXAHEDRAL+GRIDS | Search HEXAHEDRAL+GRIDS |
| 4 | SINGULAR BOUNDARY INTEGRAL EQUATION | 1 | 29% | 2% | 2 | Search SINGULAR+BOUNDARY+INTEGRAL+EQUATION | Search SINGULAR+BOUNDARY+INTEGRAL+EQUATION |
| 5 | EFFECT OF VISCOSITY | 0 | 33% | 1% | 1 | Search EFFECT+OF+VISCOSITY | Search EFFECT+OF+VISCOSITY |
| 6 | HIGH ORDER BEM | 0 | 33% | 1% | 1 | Search HIGH+ORDER+BEM | Search HIGH+ORDER+BEM |
| 7 | MODIFIED SHAPE FUNCTIONS | 0 | 33% | 1% | 1 | Search MODIFIED+SHAPE+FUNCTIONS | Search MODIFIED+SHAPE+FUNCTIONS |
| 8 | SURFACE TENSION FLOW | 0 | 33% | 1% | 1 | Search SURFACE+TENSION+FLOW | Search SURFACE+TENSION+FLOW |
| 9 | TURBULENT PULSATION | 0 | 33% | 1% | 1 | Search TURBULENT+PULSATION | Search TURBULENT+PULSATION |
| 10 | VELOCITY HEAD | 0 | 33% | 1% | 1 | Search VELOCITY+HEAD | Search VELOCITY+HEAD |
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 | PANEL METHODS | 2 | 40% | 4% | 4 |
| 2 | KINETIC FIELD | 1 | 100% | 2% | 2 |
| 3 | MEGAFLOW | 0 | 33% | 1% | 1 |
| 4 | STRUCTURED MESHES | 0 | 33% | 1% | 1 |
| 5 | KUTTA CONDITION | 0 | 14% | 2% | 2 |
| 6 | VISCEL PROJECT | 0 | 14% | 1% | 1 |
| 7 | DIPOLAR BODIES | 0 | 10% | 1% | 1 |
| 8 | AEROHYDRODYNAMICS | 0 | 100% | 1% | 1 |
| 9 | ORDER PANEL METHODS | 0 | 100% | 1% | 1 |
| 10 | SUBSONIC AERODYNAMIC CHARACTERISTICS | 0 | 100% | 1% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Experience in integrating CFD to the technology of testing models in wind tunnels | 1998 | 4 | 1 | 100% |
| Computational tools for supporting the testing of civil aircraft configurations in wind tunnels | 2008 | 7 | 12 | 42% |
| Conception of electronic wind tunnel and first results of its implementation | 2001 | 3 | 5 | 20% |
| STUDIES IN JAPAN ON CIRCULAR CASCADES COMPOSED OF THICK VANES | 1988 | 0 | 5 | 80% |
| Navier-Stokes solvers in European aircraft design | 2002 | 33 | 39 | 3% |
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 | DIPARTIMENTO METODI MODELLI MATEMAT SCI PLIC | 1 | 50% | 1.1% | 1 |
| 2 | POWER UNIT | 1 | 50% | 1.1% | 1 |
| 3 | EADS MIL AIRCRAFT | 0 | 33% | 1.1% | 1 |
| 4 | ESA 7067 | 0 | 20% | 1.1% | 1 |
| 5 | ENERGET MECAN FLUIDES INTERNE | 0 | 17% | 1.1% | 1 |
| 6 | MACHINE MECH | 0 | 17% | 1.1% | 1 |
| 7 | PSEB | 0 | 11% | 1.1% | 1 |
| 8 | CHEBOTAREV SCI MATH MECH | 0 | 100% | 1.1% | 1 |
| 9 | CNRSLMFI | 0 | 100% | 1.1% | 1 |
| 10 | URA UP | 0 | 100% | 1.1% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000152040 | EXIT TIME PROBLEM//ERROR SQUARED CONTROLLER//PROGRAMA POS STRICTO SENSU MODELAGEM MATEMAT |
| 2 | 0.0000146831 | GROUND EFFECT//WING IN GROUND EFFECT//POWER AUGMENTED RAM |
| 3 | 0.0000126657 | LOCAL SUPERSONIC REGIONS//INVERSE DESIGN//AEROSP PROP GRP |
| 4 | 0.0000126493 | OSEEN FLOW//LAPLACES TIDAL EQUATION//UER MATH PU PL |
| 5 | 0.0000123781 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
| 6 | 0.0000121183 | SUPERCAVITATION//CAVITATING FLOW//VEHICLE TRANSPORTAT ENGN |
| 7 | 0.0000110212 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
| 8 | 0.0000100089 | SENSITIVITY EQUATION METHOD//CODE VERIFICATION//MANUFACTURED SOLUTIONS |
| 9 | 0.0000095960 | AUTONOMOUS AERIAL REFUELING//LATERAL INHIBITION LI//AERIAL REFUELING |
| 10 | 0.0000091758 | MOMENTUM INJECTION//CLAUSER TECHNIQUE//DEEP WATER RISERS |