Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
14890 | 674 | 18.0 | 22% |
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 | LOCAL SUPERSONIC REGIONS | Author keyword | 6 | 71% | 1% | 5 |
2 | INVERSE DESIGN | Author keyword | 5 | 21% | 3% | 21 |
3 | AEROSP PROP GRP | Address | 3 | 100% | 0% | 3 |
4 | BALL SPINE ALGORITHM | Author keyword | 3 | 100% | 0% | 3 |
5 | LIN REISSNER TSIEN EQUATION | Author keyword | 2 | 67% | 0% | 2 |
6 | LOCAL SUPERSONIC ZONES | Author keyword | 2 | 67% | 0% | 2 |
7 | BLADE FORCE | Author keyword | 2 | 50% | 0% | 3 |
8 | COMPRESSOR BLADE PROFILE | Author keyword | 1 | 100% | 0% | 2 |
9 | DESIGN OPTIMUM SYST DOS | Address | 1 | 100% | 0% | 2 |
10 | DISTRIBUTED LOSS MODEL | Author keyword | 1 | 100% | 0% | 2 |
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 | LOCAL SUPERSONIC REGIONS | 6 | 71% | 1% | 5 | Search LOCAL+SUPERSONIC+REGIONS | Search LOCAL+SUPERSONIC+REGIONS |
2 | INVERSE DESIGN | 5 | 21% | 3% | 21 | Search INVERSE+DESIGN | Search INVERSE+DESIGN |
3 | BALL SPINE ALGORITHM | 3 | 100% | 0% | 3 | Search BALL+SPINE+ALGORITHM | Search BALL+SPINE+ALGORITHM |
4 | LIN REISSNER TSIEN EQUATION | 2 | 67% | 0% | 2 | Search LIN+REISSNER+TSIEN+EQUATION | Search LIN+REISSNER+TSIEN+EQUATION |
5 | LOCAL SUPERSONIC ZONES | 2 | 67% | 0% | 2 | Search LOCAL+SUPERSONIC+ZONES | Search LOCAL+SUPERSONIC+ZONES |
6 | BLADE FORCE | 2 | 50% | 0% | 3 | Search BLADE+FORCE | Search BLADE+FORCE |
7 | COMPRESSOR BLADE PROFILE | 1 | 100% | 0% | 2 | Search COMPRESSOR+BLADE+PROFILE | Search COMPRESSOR+BLADE+PROFILE |
8 | DISTRIBUTED LOSS MODEL | 1 | 100% | 0% | 2 | Search DISTRIBUTED+LOSS+MODEL | Search DISTRIBUTED+LOSS+MODEL |
9 | DUAL STREAM FUNCTIONS | 1 | 50% | 0% | 2 | Search DUAL+STREAM+FUNCTIONS | Search DUAL+STREAM+FUNCTIONS |
10 | FLEXIBLE STRING ALGORITHM | 1 | 100% | 0% | 2 | Search FLEXIBLE+STRING+ALGORITHM | Search FLEXIBLE+STRING+ALGORITHM |
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 | FLEXIBLE STRING ALGORITHM | 6 | 71% | 1% | 5 |
2 | BLADE DESIGN | 5 | 33% | 2% | 12 |
3 | 3 DIMENSIONAL INVERSE METHOD | 4 | 75% | 0% | 3 |
4 | SINGULAR INTEGRAL TRANSFORMS | 3 | 100% | 0% | 3 |
5 | 3 DIMENSIONAL INVERSE DESIGN | 2 | 67% | 0% | 2 |
6 | TURBO ROTOR | 2 | 67% | 0% | 2 |
7 | AERODYNAMIC DESIGN | 2 | 18% | 1% | 10 |
8 | NAVIER STOKES SOLVER | 2 | 31% | 1% | 5 |
9 | FULL POTENTIAL EQUATION | 2 | 43% | 0% | 3 |
10 | STREAM FUNCTION | 2 | 24% | 1% | 6 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references | % act. ref. to same field |
---|---|---|---|---|
Non-unique transonic flows over airfoils | 2012 | 2 | 11 | 100% |
COMPUTATIONAL METHODS FOR AERODYNAMIC SHAPE DESIGN | 1994 | 8 | 33 | 88% |
Transonic flow computations using nonlinear potential methods | 2000 | 14 | 114 | 61% |
A review of streamline coordinate approach for inviscid flows | 2006 | 1 | 11 | 64% |
Transonic flow potential method development at Ames research center | 2009 | 2 | 10 | 50% |
COMPUTATIONAL METHODS FOR THE AERODYNAMIC DESIGN OF AIRCRAFT-COMPONENTS | 1993 | 20 | 4 | 25% |
A brief review of some application driven fast algorithms for elliptic partial differential equations | 2012 | 0 | 16 | 50% |
SUPERCRITICAL AIRFOIL AND WING DESIGN | 1984 | 13 | 7 | 100% |
THE COMPUTATION OF TRANSONIC POTENTIAL FLOWS | 1982 | 6 | 7 | 43% |
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 | AEROSP PROP GRP | 3 | 100% | 0.4% | 3 |
2 | DESIGN OPTIMUM SYST DOS | 1 | 100% | 0.3% | 2 |
3 | QADR AERODYNAM | 1 | 100% | 0.3% | 2 |
4 | COMPUTAT PHYS SIMULAT BRANCH | 1 | 40% | 0.3% | 2 |
5 | COMP SOR IL | 1 | 50% | 0.1% | 1 |
6 | MAIDO | 0 | 33% | 0.1% | 1 |
7 | COMMERCIAL AIRPLANE GRP | 0 | 14% | 0.1% | 1 |
8 | GERMAN AEROSPACE | 0 | 13% | 0.1% | 1 |
9 | TRANSPORT AIRCRAFT | 0 | 11% | 0.1% | 1 |
10 | NAL | 0 | 10% | 0.1% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000170015 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
2 | 0.0000142026 | ROTOR FLOWS//CONTINUOUS ADJOINT//DISCRETE ADJOINT |
3 | 0.0000126657 | CUBIC BOUNDARY ELEMENT//BALANCE RELATIONS//DIPARTIMENTO METODI MODELLI MATEMAT SCI PLIC |
4 | 0.0000109500 | BUFFET//AERODYNAM ENERGET MODELLING//SHOCK BUFFET |
5 | 0.0000105354 | AV CONTROL//AVION CONTROL//ADAPTIVE WINGS |
6 | 0.0000097775 | V WING//CONICAL FLOWS//VORTEX FERRI SINGULARITIES |
7 | 0.0000081378 | CENTRIFUGAL COMPRESSOR//VANED DIFFUSER//CROSS FLOW FAN |
8 | 0.0000074776 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//AEROHYDROMECH//THERMAL TURBOMACHINERY MACHINE DYNAM |
9 | 0.0000067126 | RESTRICTED SHOCK SEPARATION//FREE SHOCK SEPARATION//SIDE LOADS |
10 | 0.0000062772 | VECTOR AND PARALLEL COMPUTERS//HEART CELL MODEL//NETWORK ANALOGUE |