Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 30434 | 138 | 22.3 | 24% |
Classes in level above (level 2) |
| ID, lev. above |
Publications | Label for level above |
|---|---|---|
| 1556 | 6771 | ORGANIC RANKINE CYCLE//COGENERATION//DISTRICT HEATING |
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 | TRAPPED VORTEX COMBUSTOR | Author keyword | 26 | 87% | 9% | 13 |
| 2 | TRAPPED VORTEX | Author keyword | 3 | 45% | 4% | 5 |
| 3 | SCI TECHNOL AEROENGINES AEROTHERMO | Address | 2 | 67% | 1% | 2 |
| 4 | POWER PROP | Address | 2 | 16% | 9% | 12 |
| 5 | COMBUST SPRAY | Address | 2 | 33% | 4% | 5 |
| 6 | INTERCOOLING | Author keyword | 1 | 21% | 4% | 6 |
| 7 | CAVITY COMBUSTOR | Author keyword | 1 | 50% | 1% | 2 |
| 8 | MODIFIED EDDY DISSIPATION CONCEPT | Author keyword | 1 | 100% | 1% | 2 |
| 9 | REVERSED FLOW CORE | Author keyword | 1 | 100% | 1% | 2 |
| 10 | TURBINE BURNER | Author keyword | 1 | 100% | 1% | 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 | TRAPPED VORTEX COMBUSTOR | 26 | 87% | 9% | 13 | Search TRAPPED+VORTEX+COMBUSTOR | Search TRAPPED+VORTEX+COMBUSTOR |
| 2 | TRAPPED VORTEX | 3 | 45% | 4% | 5 | Search TRAPPED+VORTEX | Search TRAPPED+VORTEX |
| 3 | INTERCOOLING | 1 | 21% | 4% | 6 | Search INTERCOOLING | Search INTERCOOLING |
| 4 | CAVITY COMBUSTOR | 1 | 50% | 1% | 2 | Search CAVITY+COMBUSTOR | Search CAVITY+COMBUSTOR |
| 5 | MODIFIED EDDY DISSIPATION CONCEPT | 1 | 100% | 1% | 2 | Search MODIFIED+EDDY+DISSIPATION+CONCEPT | Search MODIFIED+EDDY+DISSIPATION+CONCEPT |
| 6 | REVERSED FLOW CORE | 1 | 100% | 1% | 2 | Search REVERSED+FLOW+CORE | Search REVERSED+FLOW+CORE |
| 7 | TURBINE BURNER | 1 | 100% | 1% | 2 | Search TURBINE+BURNER | Search TURBINE+BURNER |
| 8 | MOMENTUM FLUX RATIO | 1 | 25% | 3% | 4 | Search MOMENTUM+FLUX+RATIO | Search MOMENTUM+FLUX+RATIO |
| 9 | AUGMENTOR | 1 | 50% | 1% | 1 | Search AUGMENTOR | Search AUGMENTOR |
| 10 | CAVITY STABILIZED FLAME | 1 | 50% | 1% | 1 | Search CAVITY+STABILIZED+FLAME | Search CAVITY+STABILIZED+FLAME |
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 | PERFORMANCE INCREASES | 15 | 88% | 5% | 7 |
| 2 | GAS TURBINE AEROENGINES | 7 | 67% | 4% | 6 |
| 3 | TRAPPED VORTEX COMBUSTOR | 2 | 33% | 4% | 5 |
| 4 | NONPREMIXED COMBUSTION | 1 | 25% | 4% | 5 |
| 5 | TURBINE BURNERS | 1 | 100% | 1% | 2 |
| 6 | FLAME BURNER | 1 | 50% | 1% | 1 |
| 7 | THERMAL INTENSITY | 1 | 50% | 1% | 1 |
| 8 | TURBOFAN ENGINE | 0 | 14% | 2% | 3 |
| 9 | EDDY DISSIPATION CONCEPT | 0 | 33% | 1% | 1 |
| 10 | VORTEX COMBUSTOR DYNAMICS | 0 | 33% | 1% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Stationary gas turbines and primary energies: A review of fuel influence on energy and combustion performances | 2000 | 12 | 5 | 80% |
| The utilization of recuperated and regenerated engine cycles for high-efficiency gas turbines in the 21st century | 1996 | 40 | 3 | 33% |
| Data and performances of selected aircraft and rotorcraft | 2000 | 7 | 4 | 25% |
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 | SCI TECHNOL AEROENGINES AEROTHERMO | 2 | 67% | 1.4% | 2 |
| 2 | POWER PROP | 2 | 16% | 8.7% | 12 |
| 3 | COMBUST SPRAY | 2 | 33% | 3.6% | 5 |
| 4 | FLUID DYNAMICS | 1 | 50% | 0.7% | 1 |
| 5 | FUELS LUBRICAT | 1 | 50% | 0.7% | 1 |
| 6 | TEAM LEAD TECHNOL ROTATING EQUIPMENT | 1 | 50% | 0.7% | 1 |
| 7 | POWER ENGN PROPULS | 0 | 33% | 0.7% | 1 |
| 8 | HIGH PERFORMANCE COMP MODERNIZAT PROGRAM | 0 | 17% | 0.7% | 1 |
| 9 | SCI TECHNOL AEROENGINE AEROTHERM | 0 | 17% | 0.7% | 1 |
| 10 | AERONAUT PROP | 0 | 14% | 0.7% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000272432 | WAVE ROTOR//MICRO SHOCK TUBE//PRESSURE WAVE SUPERCHARGER |
| 2 | 0.0000143119 | GAS PATH ANALYSIS//AVIAT MOTOR CONTROL SYST//GAS PATH DIAGNOSTICS |
| 3 | 0.0000121676 | INLET AIR COOLING//HEAT RECOVERY STEAM GENERATOR//EXERGOECONOMICS |
| 4 | 0.0000120226 | TURBO MACHINERY//COMPOUND CHOKING//COMPOUND WAVES |
| 5 | 0.0000108650 | SIDE DUMP COMBUSTOR//COMBUSTOR FLOW//JET IMPINGEMENTS |
| 6 | 0.0000106342 | MILD COMBUSTION//FLAMELESS COMBUSTION//FLAMELESS OXIDATION |
| 7 | 0.0000097714 | ANNULAR DIFFUSER//SUBSONIC WIND TUNNEL//EXHAUST HOOD |
| 8 | 0.0000081585 | PLATE HEAT EXCHANGER//PLATE HEAT EXCHANGERS//FLOW MALDISTRIBUTION |
| 9 | 0.0000081136 | SCRAMJET//SUPERSONIC COMBUSTION//JOURNAL OF PROPULSION AND POWER |
| 10 | 0.0000078161 | SURVEILLANCE SENSOR//INFRARED SIGNATURE//ABSOLUTE SPECTRAL RADIANT EXITANCE |