Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
19989 | 417 | 22.8 | 27% |
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 | CONFIGURAT AERODYNAM BRANCH | Address | 13 | 47% | 5% | 21 |
2 | AVIAT PROGRAM GRP | Address | 10 | 43% | 4% | 18 |
3 | CIVIL TRANSPORT TEAM | Address | 8 | 100% | 1% | 5 |
4 | CIVIL AIRCRAFT UNIT | Address | 6 | 71% | 1% | 5 |
5 | SUPERSON TRANSPORT TEAM | Address | 3 | 60% | 1% | 3 |
6 | AERONAUT SYST ANAL BRANCH | Address | 3 | 42% | 1% | 5 |
7 | TRANSPORT AIRCRAFT | Address | 2 | 44% | 1% | 4 |
8 | ISENTROPIC COMPRESSION FLOWS | Author keyword | 2 | 67% | 0% | 2 |
9 | MULTIDISCIPLINARY DESIGN EXPLORATION | Author keyword | 2 | 67% | 0% | 2 |
10 | OVERSET UNSTRUCTURED GRIDS | Author keyword | 2 | 67% | 0% | 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 | SURFACE TRIANGULATION | 25 | 71% | 5% | 20 |
2 | 3 DIMENSIONAL FLOWFIELD COMPUTATIONS | 11 | 78% | 2% | 7 |
3 | EULER METHODS | 8 | 70% | 2% | 7 |
4 | WAKE INTEGRATION | 8 | 75% | 1% | 6 |
5 | ADVANCING LAYERS METHOD | 6 | 100% | 1% | 4 |
6 | DRAG PREDICTION WORKSHOP | 3 | 57% | 1% | 4 |
7 | NUMERICAL AERODYNAMICS | 3 | 100% | 1% | 3 |
8 | TIP SAILS | 2 | 67% | 0% | 2 |
9 | TRANSONIC TRANSPORT | 1 | 100% | 0% | 2 |
10 | WING BODY CONFIGURATION | 1 | 100% | 0% | 2 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Supersonic biplane-A review | 2011 | 5 | 10 | 80% |
Supersonic drag reduction technology in the scaled supersonic experimental airplane project by JAXA | 2009 | 4 | 6 | 83% |
Drag due to lift: Concepts for prediction and reduction | 2001 | 45 | 10 | 40% |
Shock wave drag reduction | 2004 | 14 | 16 | 56% |
A short history of the European Transonic Wind Tunnel ETW | 2011 | 2 | 2 | 50% |
Recent experience with different methods of drag prediction | 1999 | 37 | 35 | 29% |
A review of ONERA aerodynamic research in support of a future supersonic transport aircraft | 2000 | 5 | 3 | 67% |
Aircraft drag reduction - a review | 2003 | 11 | 49 | 24% |
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 | CONFIGURAT AERODYNAM BRANCH | 13 | 47% | 5.0% | 21 |
2 | AVIAT PROGRAM GRP | 10 | 43% | 4.3% | 18 |
3 | CIVIL TRANSPORT TEAM | 8 | 100% | 1.2% | 5 |
4 | CIVIL AIRCRAFT UNIT | 6 | 71% | 1.2% | 5 |
5 | SUPERSON TRANSPORT TEAM | 3 | 60% | 0.7% | 3 |
6 | AERONAUT SYST ANAL BRANCH | 3 | 42% | 1.2% | 5 |
7 | TRANSPORT AIRCRAFT | 2 | 44% | 1.0% | 4 |
8 | PL AERODYNAM | 2 | 12% | 3.4% | 14 |
9 | AVIAT PROGRAM | 1 | 100% | 0.5% | 2 |
10 | COMPUTAT AEROSCI BRANCH | 1 | 11% | 1.9% | 8 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000276657 | ROTOR FLOWS//CONTINUOUS ADJOINT//DISCRETE ADJOINT |
2 | 0.0000186993 | AV CONTROL//AVION CONTROL//ADAPTIVE WINGS |
3 | 0.0000139005 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
4 | 0.0000127523 | ANOMALOUS TRANSPARENCY//SHOOTING ARGUMENTS//GENERALIZED BURGERS EQUATION |
5 | 0.0000123781 | CUBIC BOUNDARY ELEMENT//BALANCE RELATIONS//DIPARTIMENTO METODI MODELLI MATEMAT SCI PLIC |
6 | 0.0000115446 | CARBUNCLE PHENOMENON//SHOCK INSTABILITY//MACH UNIFORM |
7 | 0.0000109827 | SENSITIVITY EQUATION METHOD//CODE VERIFICATION//MANUFACTURED SOLUTIONS |
8 | 0.0000103153 | GLENN L MARTIN TECHNOL//JOURNAL OF THE AMERICAN HELICOPTER SOCIETY//ROTOR FUSELAGE INTERACTION |
9 | 0.0000103044 | BUFFET//AERODYNAM ENERGET MODELLING//SHOCK BUFFET |
10 | 0.0000087716 | MESH GENERATION//MESH QUALITY//ENGINEERING WITH COMPUTERS |