Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
4019 | 1788 | 23.2 | 35% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
279 | 18428 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW//FILM COOLING |
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 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | Journal | 224 | 27% | 40% | 721 |
2 | FILM COOLING | Author keyword | 158 | 56% | 11% | 191 |
3 | FILM COOLING EFFECTIVENESS | Author keyword | 47 | 68% | 2% | 41 |
4 | TURBINE HEAT TRANSFER | Address | 29 | 49% | 2% | 42 |
5 | CONVERGING SLOT HOLE | Author keyword | 17 | 100% | 0% | 8 |
6 | BLOWING RATIO | Author keyword | 16 | 51% | 1% | 22 |
7 | TURBINE SYST | Address | 15 | 71% | 1% | 12 |
8 | AERODYNAMIC LOSS | Author keyword | 13 | 67% | 1% | 12 |
9 | COMPOUND ANGLE | Author keyword | 12 | 75% | 1% | 9 |
10 | PASSAGE VORTEX | Author keyword | 11 | 78% | 0% | 7 |
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 | FILM COOLING | 158 | 56% | 11% | 191 | Search FILM+COOLING | Search FILM+COOLING |
2 | FILM COOLING EFFECTIVENESS | 47 | 68% | 2% | 41 | Search FILM+COOLING+EFFECTIVENESS | Search FILM+COOLING+EFFECTIVENESS |
3 | CONVERGING SLOT HOLE | 17 | 100% | 0% | 8 | Search CONVERGING+SLOT+HOLE | Search CONVERGING+SLOT+HOLE |
4 | BLOWING RATIO | 16 | 51% | 1% | 22 | Search BLOWING+RATIO | Search BLOWING+RATIO |
5 | AERODYNAMIC LOSS | 13 | 67% | 1% | 12 | Search AERODYNAMIC+LOSS | Search AERODYNAMIC+LOSS |
6 | COMPOUND ANGLE | 12 | 75% | 1% | 9 | Search COMPOUND+ANGLE | Search COMPOUND+ANGLE |
7 | PASSAGE VORTEX | 11 | 78% | 0% | 7 | Search PASSAGE+VORTEX | Search PASSAGE+VORTEX |
8 | COOLING EFFECTIVENESS | 10 | 39% | 1% | 20 | Search COOLING+EFFECTIVENESS | Search COOLING+EFFECTIVENESS |
9 | ENDWALL HEAT TRANSFER | 9 | 83% | 0% | 5 | Search ENDWALL+HEAT+TRANSFER | Search ENDWALL+HEAT+TRANSFER |
10 | ADIABATIC EFFECTIVENESS | 9 | 59% | 1% | 10 | Search ADIABATIC+EFFECTIVENESS | Search ADIABATIC+EFFECTIVENESS |
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 | CRYSTAL IMAGE METHOD | 50 | 88% | 1% | 23 |
2 | COMPOUND ANGLE HOLES | 39 | 68% | 2% | 34 |
3 | 2 STAGGERED ROWS | 37 | 100% | 1% | 14 |
4 | SHAPED HOLES | 32 | 57% | 2% | 39 |
5 | EXPANDED EXITS | 31 | 71% | 1% | 25 |
6 | ADIABATIC EFFECTIVENESS | 29 | 75% | 1% | 21 |
7 | FULL STAGE TURBINE | 27 | 83% | 1% | 15 |
8 | 2 ROWS | 25 | 73% | 1% | 19 |
9 | RESULTS DOWNSTREAM | 22 | 68% | 1% | 19 |
10 | SQUEALER TIP | 19 | 60% | 1% | 21 |
Journals |
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 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 224 | 27% | 40% | 721 |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
A review of shaped hole turbine film-cooling technology | 2005 | 191 | 7 | 100% |
Gas turbine heat transfer: Ten remaining hot gas path challenges | 2007 | 38 | 5 | 60% |
Turbine endwall aerodynamics and heat transfer | 2006 | 27 | 34 | 91% |
A review of gas turbine effusion cooling studies | 2013 | 1 | 22 | 73% |
Combustion and cooling performance in an aero-engine annular combustor | 2006 | 11 | 3 | 67% |
Problems of and prospects for the investigation of the thermal conditions of blades of high-temperature gas turbines (a review based on presentations to the Third Russian National Conference on Heat Transfer) | 2003 | 0 | 3 | 100% |
PROGRESS TOWARDS UNDERSTANDING AND PREDICTING HEAT-TRANSFER IN THE TURBINE GAS PATH | 1993 | 32 | 65 | 57% |
Role of solar wind turbulence in the coupling of the solar wind to the Earth's magnetosphere | 2003 | 63 | 69 | 7% |
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 | TURBINE HEAT TRANSFER | 29 | 49% | 2.3% | 42 |
2 | TURBINE SYST | 15 | 71% | 0.7% | 12 |
3 | WHITTLE | 10 | 20% | 2.5% | 44 |
4 | OSNEY | 7 | 67% | 0.3% | 6 |
5 | PRATT WHITNEY AIRCRAFT | 6 | 80% | 0.2% | 4 |
6 | TURBINES BRANCH | 6 | 80% | 0.2% | 4 |
7 | AYT CORP | 6 | 71% | 0.3% | 5 |
8 | LEHRSTUHL THERM STROMUNGSMA INEN | 6 | 33% | 0.8% | 15 |
9 | TURBINE AERODYNAM | 5 | 60% | 0.3% | 6 |
10 | THERM STROMUNGSMA INEN | 5 | 26% | 1.0% | 18 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000189421 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//LAMINAR SEPARATION BUBBLE//SEPARATED FLOW TRANSITION |
2 | 0.0000189196 | ENERGY CONVERS CONSERVAT//MIST COOLING//CONJUGATE HEAT TRANSFER METHODOLOGY |
3 | 0.0000174342 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//AEROHYDROMECH//THERMAL TURBOMACHINERY MACHINE DYNAM |
4 | 0.0000172944 | SURFACE SHEAR STRESS MEASUREMENT//THERMOCHROMIC LIQUID CRYSTALS//LIQUID CRYSTAL COATING |
5 | 0.0000161821 | JETS IN CROSSFLOW//JET IN CROSS FLOW//JET IN CROSSFLOW |
6 | 0.0000124072 | TRANSPIRATION COOLING//UMR 5008 THERM LYON//COMPRESSIBLE OR INCOMPRESSIBLE FLUID |
7 | 0.0000094290 | ROTOR STATOR CAVITY//ROTOR STATOR SYSTEM//THERMOFLUID SYST UTC |
8 | 0.0000076906 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//CASING TREATMENT//ROTATING STALL |
9 | 0.0000069857 | ARTIFICIAL ROUGHNESS//TURBINE HEAT TRANSFER//SOLAR AIR HEATER |
10 | 0.0000064294 | HEAT FLUX GAGE//MICRO C OUEST//NON INTEGER SYSTEM IDENTIFICATION |