Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
31299 | 125 | 23.2 | 24% |
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 | OPERATOR DIFFERENCE SCHEMES | Author keyword | 8 | 62% | 6% | 8 |
2 | FINITE VOLUME TIME DOMAIN | Author keyword | 4 | 75% | 2% | 3 |
3 | CYLINDRICAL HOUSING | Author keyword | 2 | 67% | 2% | 2 |
4 | FIRST ORDER EVOLUTIONARY EQUATION | Author keyword | 2 | 67% | 2% | 2 |
5 | SPLITTING SCHEMES | Author keyword | 2 | 29% | 5% | 6 |
6 | ADDITIVE OPERATOR DIFFERENCE SCHEMES | Author keyword | 1 | 100% | 2% | 2 |
7 | CLASSICAL HYPERSONIC BOUNDARY LAYER EQUATIONS | Author keyword | 1 | 100% | 2% | 2 |
8 | HYPERSONIC KINETIC BOUNDARY LAYER EQUATIONS | Author keyword | 1 | 100% | 2% | 2 |
9 | MATHEMATICAL SIMULATION METHODS | Author keyword | 1 | 100% | 2% | 2 |
10 | STABILITY OF OPERATOR DIFFERENCE SCHEMES | Author keyword | 1 | 100% | 2% | 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 | CHARACTERISTIC BASED ALGORITHMS | 4 | 75% | 2% | 3 |
2 | AEROASSIST FLIGHT EXPERIMENT | 2 | 67% | 2% | 2 |
3 | KINETIC THEORY DESCRIPTION | 1 | 50% | 1% | 1 |
4 | BLUNT BODY FLOW | 0 | 20% | 1% | 1 |
5 | NAVIER STOKES CODE | 0 | 20% | 1% | 1 |
6 | BLUNT NOSED BODY | 0 | 100% | 1% | 1 |
7 | EXPERIMENT VEHICLE | 0 | 100% | 1% | 1 |
8 | LANCHESTER MEMORIAL LECTURE | 0 | 100% | 1% | 1 |
9 | REAL GAS HYPERSONICS | 0 | 100% | 1% | 1 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Lester lees and hypersonic aerodynamics | 2003 | 0 | 3 | 67% |
PERSPECTIVE ON HYPERSONIC NONEQUILIBRIUM-FLOW | 1995 | 22 | 21 | 24% |
Computational fluid dynamics application to aerospace science | 2009 | 4 | 61 | 15% |
Shared knowledge in computational fluid dynamics, electromagnetics, and magneto-aerodynamics | 2002 | 10 | 21 | 19% |
Three decades of accomplishments in computational fluid dynamics | 2004 | 12 | 38 | 13% |
PERSPECTIVES ON HYPERSONIC VISCOUS-FLOW RESEARCH | 1993 | 22 | 44 | 14% |
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 | ILIA VEKUA PL MATH | 0 | 33% | 0.8% | 1 |
2 | INDIAN AIR FORCE | 0 | 25% | 0.8% | 1 |
3 | RADAR ELECT WARFARE SECT | 0 | 25% | 0.8% | 1 |
4 | MAGNET FIELD CONTROL PLICAT | 0 | 10% | 0.8% | 1 |
5 | EXELLENCE COMP SIMULAT | 0 | 100% | 0.8% | 1 |
6 | MULTIPHASE FLOW VISUAL ANAL | 0 | 100% | 0.8% | 1 |
7 | NUCL POWER ENGN DEV SAFETY PROBLEMS | 0 | 100% | 0.8% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000140695 | V WING//CONICAL FLOWS//VORTEX FERRI SINGULARITIES |
2 | 0.0000138328 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
3 | 0.0000116096 | SENSITIVITY EQUATION METHOD//CODE VERIFICATION//MANUFACTURED SOLUTIONS |
4 | 0.0000105911 | AEROTHERMODYNAM BRANCH//JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER//REACTING FLOW ENVIRONM BRANCH |
5 | 0.0000090147 | PLASMA ACTUATORS//SCI TECHNOL PLASMA DYNAM//PLASMA AERODYNAMIC ACTUATION |
6 | 0.0000087224 | DISK MHD GENERATOR//IDO SCHEME//MHD POWER GENERATION |
7 | 0.0000080348 | CONSTRAINED TRANSPORT//EVOLUTION GALERKIN SCHEMES//GENUINELY MULTIDIMENSIONAL SCHEMES |
8 | 0.0000079365 | MAC BRIDGE//EXTENDED LAN//SHOP FLOOR INTEGRATION SYSTEM |
9 | 0.0000078773 | BIRD STRIKE//TENSOR SKIN//SOFT BODY IMPACT |
10 | 0.0000077842 | TRANSPIRATION COOLING//UMR 5008 THERM LYON//COMPRESSIBLE OR INCOMPRESSIBLE FLUID |