Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 16702 | 575 | 20.2 | 25% |
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 | ANNULAR DIFFUSER | Author keyword | 4 | 67% | 1% | 4 |
| 2 | SUBSONIC WIND TUNNEL | Author keyword | 3 | 57% | 1% | 4 |
| 3 | EXHAUST HOOD | Author keyword | 3 | 43% | 1% | 6 |
| 4 | CO AXIAL JETS | Author keyword | 3 | 100% | 1% | 3 |
| 5 | AERO ENGINE COMBUSTOR | Author keyword | 3 | 60% | 1% | 3 |
| 6 | DUMP COMBUSTOR | Author keyword | 2 | 33% | 1% | 6 |
| 7 | TURBULENT FLOW FIELDS | Author keyword | 2 | 67% | 0% | 2 |
| 8 | X PROBE | Author keyword | 2 | 50% | 1% | 3 |
| 9 | CHUTE MIXER | Author keyword | 1 | 100% | 0% | 2 |
| 10 | FUEL ITERATIVE APPROXIMATION | 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 | ANNULAR DIFFUSER | 4 | 67% | 1% | 4 | Search ANNULAR+DIFFUSER | Search ANNULAR+DIFFUSER |
| 2 | SUBSONIC WIND TUNNEL | 3 | 57% | 1% | 4 | Search SUBSONIC+WIND+TUNNEL | Search SUBSONIC+WIND+TUNNEL |
| 3 | EXHAUST HOOD | 3 | 43% | 1% | 6 | Search EXHAUST+HOOD | Search EXHAUST+HOOD |
| 4 | CO AXIAL JETS | 3 | 100% | 1% | 3 | Search CO+AXIAL+JETS | Search CO+AXIAL+JETS |
| 5 | AERO ENGINE COMBUSTOR | 3 | 60% | 1% | 3 | Search AERO+ENGINE+COMBUSTOR | Search AERO+ENGINE+COMBUSTOR |
| 6 | DUMP COMBUSTOR | 2 | 33% | 1% | 6 | Search DUMP+COMBUSTOR | Search DUMP+COMBUSTOR |
| 7 | TURBULENT FLOW FIELDS | 2 | 67% | 0% | 2 | Search TURBULENT+FLOW+FIELDS | Search TURBULENT+FLOW+FIELDS |
| 8 | X PROBE | 2 | 50% | 1% | 3 | Search X+PROBE | Search X+PROBE |
| 9 | CHUTE MIXER | 1 | 100% | 0% | 2 | Search CHUTE+MIXER | Search CHUTE+MIXER |
| 10 | FUEL ITERATIVE APPROXIMATION | 1 | 100% | 0% | 2 | Search FUEL+ITERATIVE+APPROXIMATION | Search FUEL+ITERATIVE+APPROXIMATION |
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 | COMPRESSOR EXIT CONDITIONS | 8 | 62% | 1% | 8 |
| 2 | ANNULAR DIFFUSERS | 5 | 54% | 1% | 7 |
| 3 | WEAK EXTINCTION LIMITS | 3 | 60% | 1% | 3 |
| 4 | GAS TURBINE COMBUSTOR | 3 | 16% | 3% | 15 |
| 5 | CENTRAL LOBED MIXER | 2 | 67% | 0% | 2 |
| 6 | COMBUSTOR ANNULAR DIFFUSERS | 1 | 38% | 1% | 3 |
| 7 | LEAN BLOW OUT | 1 | 100% | 0% | 2 |
| 8 | BODY FLAME STABILIZER | 1 | 50% | 0% | 1 |
| 9 | CROSS STREAM | 1 | 50% | 0% | 1 |
| 10 | RESEARCH COMBUSTOR | 1 | 50% | 0% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| CHARACTERISTICS OF COMBUSTOR DIFFUSERS | 1995 | 29 | 15 | 67% |
| APPLICATION OF ROOF RADIANT BURNERS IN LARGE PUSHER-TYPE FURNACES | 2009 | 1 | 2 | 100% |
| A Literature Review of Low Pressure Steam Turbine Exhaust Hood and Diffuser Studies | 2013 | 0 | 14 | 86% |
| MODELING OF SWIRL IN TURBULENT-FLOW SYSTEMS | 1986 | 146 | 19 | 32% |
| COMBUSTION-GENERATED TURBULENCE IN PRACTICAL COMBUSTORS | 1988 | 3 | 16 | 38% |
| SEMI-EMPIRICAL CORRELATIONS FOR GAS-TURBINE EMISSIONS, IGNITION, AND FLAME STABILIZATION | 1980 | 15 | 1 | 100% |
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 | ALSTOM SWITZERLAND LTD | 1 | 50% | 0.2% | 1 |
| 2 | ENGINE PERFORMANCE | 1 | 50% | 0.2% | 1 |
| 3 | CHINA GAS TURBINE ESTAB | 0 | 33% | 0.2% | 1 |
| 4 | COMBUST TECHNOL BRANCH | 0 | 33% | 0.2% | 1 |
| 5 | ELECT POWER GENERAT | 0 | 33% | 0.2% | 1 |
| 6 | ROLLS ROYCE TECHNOL | 0 | 18% | 0.3% | 2 |
| 7 | AERONAUT AUTOMAT ENGN | 0 | 17% | 0.3% | 2 |
| 8 | AVIAT SPACE TECHNOL | 0 | 14% | 0.3% | 2 |
| 9 | AERO AUTO ENGN | 0 | 25% | 0.2% | 1 |
| 10 | AERONAUT AUTOMOT | 0 | 25% | 0.2% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000257698 | SIDE DUMP COMBUSTOR//COMBUSTOR FLOW//JET IMPINGEMENTS |
| 2 | 0.0000156534 | JETS IN CROSSFLOW//JET IN CROSS FLOW//JET IN CROSSFLOW |
| 3 | 0.0000133008 | COMBUSTION INSTABILITIES//FLAME TRANSFER FUNCTION//COMBUSTION INSTABILITY |
| 4 | 0.0000097714 | TRAPPED VORTEX COMBUSTOR//TRAPPED VORTEX//SCI TECHNOL AEROENGINES AEROTHERMO |
| 5 | 0.0000088551 | SECOND MOMENT CLOSURE//ELLIPTIC RELAXATION//TURBULENCE MODELLING |
| 6 | 0.0000082630 | CONDITIONAL MOMENT CLOSURE//MULTIPLE MAPPING CONDITIONING//TRANSPORTED PDF |
| 7 | 0.0000074123 | BACKWARD FACING STEP//FORWARD FACING STEP//SEPARATED AND REATTACHED FLOW |
| 8 | 0.0000065973 | VORTEX BREAKDOWN//COMPOUND VORTEX//SWIRLING JET |
| 9 | 0.0000063202 | TWISTED TAPE//TWISTED TAPE INSERTS//SWIRL FLOW |
| 10 | 0.0000060397 | NUMERICAL HEAT TRANSFER PART B-FUNDAMENTALS//LECUSSO SCHEME//GENERAL CURVILINEAR CO ORDINATES |