Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 25799 | 224 | 24.5 | 32% |
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 | SENSITIVITY EQUATION METHOD | Author keyword | 6 | 80% | 2% | 4 |
| 2 | CODE VERIFICATION | Author keyword | 4 | 26% | 5% | 12 |
| 3 | MANUFACTURED SOLUTIONS | Author keyword | 3 | 40% | 3% | 6 |
| 4 | MANUFACTURED SOLUTION | Author keyword | 3 | 60% | 1% | 3 |
| 5 | NODAL DERIVATIVES | Author keyword | 2 | 67% | 1% | 2 |
| 6 | NODE DISPLACEMENT | Author keyword | 2 | 67% | 1% | 2 |
| 7 | INTERDISCIPLINARY PL MATH | Address | 1 | 13% | 4% | 10 |
| 8 | BOUNDARY DERIVATIVES | Author keyword | 1 | 50% | 1% | 2 |
| 9 | CONTINUOUS SENSITIVITY EQUATION METHOD | Author keyword | 1 | 100% | 1% | 2 |
| 10 | NEAR WALL TURBULENT FLOW | Author keyword | 1 | 100% | 1% | 2 |
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 | VISCOUS INCOMPRESSIBLE FLOWS | 4 | 23% | 7% | 15 |
| 2 | MANUFACTURED SOLUTIONS | 3 | 30% | 3% | 7 |
| 3 | SENSITIVITY EQUATION METHOD | 2 | 67% | 1% | 2 |
| 4 | INCOMPRESSIBLE LAMINAR FLOWS | 1 | 100% | 1% | 2 |
| 5 | NUMERICAL ACCURACY | 1 | 40% | 1% | 2 |
| 6 | EDDY VISCOSITY MODELS | 1 | 50% | 0% | 1 |
| 7 | 4 STROKE | 0 | 33% | 0% | 1 |
| 8 | COOLING TOWER DRIFT | 0 | 33% | 0% | 1 |
| 9 | RECOVERY TECHNIQUE | 0 | 15% | 1% | 2 |
| 10 | CODE VERIFICATION | 0 | 25% | 0% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Quantification of uncertainty in computational fluid dynamics | 1997 | 313 | 35 | 14% |
| Aerodynamically balanced ailerons for a commuter aircraft | 2001 | 2 | 5 | 40% |
| Quantification of Computational Uncertainty for Molecular and Continuum Methods in Thermo-Fluid Sciences | 2011 | 0 | 62 | 16% |
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 | INTERDISCIPLINARY PL MATH | 1 | 13% | 4.5% | 10 |
| 2 | CFD PROJECTS | 1 | 50% | 0.4% | 1 |
| 3 | DESENVOLVIMENTO PROC | 1 | 50% | 0.4% | 1 |
| 4 | EESC SMM | 1 | 50% | 0.4% | 1 |
| 5 | MECH BIOMED MFG ENGN | 1 | 50% | 0.4% | 1 |
| 6 | NITC | 1 | 50% | 0.4% | 1 |
| 7 | CNRS UMR6598 | 0 | 33% | 0.4% | 1 |
| 8 | PROJECT OPALE | 0 | 33% | 0.4% | 1 |
| 9 | ENGN QUIM ENGN ALIMENTOS EQA | 0 | 25% | 0.4% | 1 |
| 10 | COMPUTAT SIMULAT DESIGN | 0 | 12% | 0.9% | 2 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000161487 | SUPERCONVERGENCE//DISCRETE DERIVATIVE GREENS FUNCTION//GOAL ORIENTED ERROR ESTIMATION |
| 2 | 0.0000128609 | MEMBRANE HYPOTHESIS//A MOLTEN CARBONATE//BENDING THEORY OF SHELLS |
| 3 | 0.0000116096 | OPERATOR DIFFERENCE SCHEMES//FINITE VOLUME TIME DOMAIN//CYLINDRICAL HOUSING |
| 4 | 0.0000109827 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
| 5 | 0.0000100089 | CUBIC BOUNDARY ELEMENT//BALANCE RELATIONS//DIPARTIMENTO METODI MODELLI MATEMAT SCI PLIC |
| 6 | 0.0000099217 | TRANSPIRATION COOLING//UMR 5008 THERM LYON//COMPRESSIBLE OR INCOMPRESSIBLE FLUID |
| 7 | 0.0000092118 | ROTOR FLOWS//CONTINUOUS ADJOINT//DISCRETE ADJOINT |
| 8 | 0.0000091786 | ADDED RESISTANCE//JOURNAL OF SHIP RESEARCH//JOURNAL OF MARINE SCIENCE AND TECHNOLOGY |
| 9 | 0.0000091172 | AUTOMATIC DIFFERENTIATION//COMPUTATIONAL DIFFERENTIATION//INTERFACE CONTRACTION |
| 10 | 0.0000088140 | RESTRICTED SHOCK SEPARATION//FREE SHOCK SEPARATION//SIDE LOADS |