Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 20396 | 400 | 18.0 | 20% |
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 | FIELD BOUNDARY ELEMENTS | Author keyword | 2 | 67% | 1% | 2 |
| 2 | CHIMERA METHODOLOGY | Author keyword | 1 | 100% | 1% | 2 |
| 3 | HIGH SPEED AERODYNAMICS | Author keyword | 1 | 50% | 1% | 2 |
| 4 | IMPLICIT HOLE CUTTING | Author keyword | 1 | 100% | 1% | 2 |
| 5 | COMPUTAT THEORET FLUID DYNAM | Address | 1 | 15% | 2% | 7 |
| 6 | FULL POTENTIAL EQUATION | Author keyword | 1 | 21% | 1% | 3 |
| 7 | COMPUTAT MECH BRANCH | Address | 1 | 50% | 0% | 1 |
| 8 | DYNAMIC OVERSET | Author keyword | 1 | 50% | 0% | 1 |
| 9 | NAVIER STOKES ALGORITHMS | Author keyword | 1 | 50% | 0% | 1 |
| 10 | TRANSONIC VISCOUS FLOW | Author keyword | 1 | 50% | 0% | 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 | FIELD BOUNDARY ELEMENTS | 2 | 67% | 1% | 2 | Search FIELD+BOUNDARY+ELEMENTS | Search FIELD+BOUNDARY+ELEMENTS |
| 2 | CHIMERA METHODOLOGY | 1 | 100% | 1% | 2 | Search CHIMERA+METHODOLOGY | Search CHIMERA+METHODOLOGY |
| 3 | HIGH SPEED AERODYNAMICS | 1 | 50% | 1% | 2 | Search HIGH+SPEED+AERODYNAMICS | Search HIGH+SPEED+AERODYNAMICS |
| 4 | IMPLICIT HOLE CUTTING | 1 | 100% | 1% | 2 | Search IMPLICIT+HOLE+CUTTING | Search IMPLICIT+HOLE+CUTTING |
| 5 | FULL POTENTIAL EQUATION | 1 | 21% | 1% | 3 | Search FULL+POTENTIAL+EQUATION | Search FULL+POTENTIAL+EQUATION |
| 6 | DYNAMIC OVERSET | 1 | 50% | 0% | 1 | Search DYNAMIC+OVERSET | Search DYNAMIC+OVERSET |
| 7 | NAVIER STOKES ALGORITHMS | 1 | 50% | 0% | 1 | Search NAVIER+STOKES+ALGORITHMS | Search NAVIER+STOKES+ALGORITHMS |
| 8 | TRANSONIC VISCOUS FLOW | 1 | 50% | 0% | 1 | Search TRANSONIC+VISCOUS+FLOW | Search TRANSONIC+VISCOUS+FLOW |
| 9 | OVERSET GRID | 0 | 15% | 1% | 3 | Search OVERSET+GRID | Search OVERSET+GRID |
| 10 | CLEARANCE GAP | 0 | 33% | 0% | 1 | Search CLEARANCE+GAP | Search CLEARANCE+GAP |
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 | FIELD PANEL METHOD | 1 | 100% | 1% | 2 |
| 2 | AEROSPACE VEHICLES | 1 | 50% | 0% | 1 |
| 3 | COARSE GRID CORRECTION | 1 | 50% | 0% | 1 |
| 4 | DETONATION COMBUSTION | 1 | 50% | 0% | 1 |
| 5 | IMPLICIT MULTIBLOCK EULER | 1 | 50% | 0% | 1 |
| 6 | FULL POTENTIAL EQUATION | 1 | 29% | 1% | 2 |
| 7 | PREDICTION WORKSHOP | 0 | 33% | 0% | 1 |
| 8 | TRANSONIC POTENTIAL FLOW | 0 | 33% | 0% | 1 |
| 9 | AIRFOIL FLOWS | 0 | 25% | 0% | 1 |
| 10 | INDUCED SHOCK WAVE | 0 | 14% | 0% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Thirty years of development and application of CFD at Boeing Commercial Airplanes, Seattle | 2005 | 21 | 10 | 60% |
| Early development of implicit methods for Computational Fluid Dynamics at NASA Ames | 2009 | 0 | 3 | 100% |
| Experience in the use of computational aerodynamics to predict store release characteristics | 2001 | 2 | 2 | 100% |
| Overset grid technology development at NASA Ames Research Center | 2009 | 15 | 11 | 27% |
| Parallel computing of overset grids for aerodynamic problems with moving objects | 2000 | 21 | 7 | 14% |
| THE ROLE OF FLOW VISUALIZATION IN THE STUDY OF AFTERBODY AND BASE FLOWS - A REVIEW | 1985 | 2 | 1 | 100% |
| SELECTED TOPICS IN THE THEORY AND PRACTICE OF COMPUTATIONAL FLUID-DYNAMICS | 1987 | 9 | 42 | 21% |
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 | COMPUTAT THEORET FLUID DYNAM | 1 | 15% | 1.8% | 7 |
| 2 | COMPUTAT MECH BRANCH | 1 | 50% | 0.3% | 1 |
| 3 | AERONAUT SYST PROGRAM | 0 | 33% | 0.3% | 1 |
| 4 | FST GRP | 0 | 33% | 0.3% | 1 |
| 5 | POWERPLANT SYST | 0 | 33% | 0.3% | 1 |
| 6 | BOEING COMMERCIAL AIRPLANES | 0 | 25% | 0.3% | 1 |
| 7 | GELLERSEN | 0 | 25% | 0.3% | 1 |
| 8 | AEROMECH FLIGHT ENGN | 0 | 12% | 0.5% | 2 |
| 9 | CTFD | 0 | 17% | 0.3% | 1 |
| 10 | MAJOR SHARED OURCE | 0 | 13% | 0.3% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000174601 | CARBUNCLE PHENOMENON//SHOCK INSTABILITY//MACH UNIFORM |
| 2 | 0.0000170753 | SUMMATION BY PARTS//SUMMATION BY PARTS OPERATORS//HIGH ORDER FINITE DIFFERENCE METHODS |
| 3 | 0.0000170015 | LOCAL SUPERSONIC REGIONS//INVERSE DESIGN//AEROSP PROP GRP |
| 4 | 0.0000152691 | AERODYNAM BRANCH//CONING MOTION//MISSILE SYST DAHLGREN |
| 5 | 0.0000152346 | V WING//CONICAL FLOWS//VORTEX FERRI SINGULARITIES |
| 6 | 0.0000139005 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
| 7 | 0.0000138328 | OPERATOR DIFFERENCE SCHEMES//FINITE VOLUME TIME DOMAIN//CYLINDRICAL HOUSING |
| 8 | 0.0000135550 | THREE DIMENSIONAL TURBULENT BOUNDARY LAYER//MEAN THREE DIMENSIONALITY//PUMP JET |
| 9 | 0.0000126824 | SEPARATION SHOCK//CLAMP BAND JOINT//SATELLITE SEPARATION |
| 10 | 0.0000120559 | DELTA WING//HIGH ANGLE OF ATTACK//DOUBLE DELTA WING |