Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 10410 | 1000 | 22.8 | 46% |
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 | BACKWARD FACING STEP | Author keyword | 40 | 38% | 8% | 84 |
| 2 | FORWARD FACING STEP | Author keyword | 6 | 48% | 1% | 10 |
| 3 | SEPARATED AND REATTACHED FLOW | Author keyword | 6 | 80% | 0% | 4 |
| 4 | LARGE SCALE VORTICAL STRUCTURE | Author keyword | 5 | 60% | 1% | 6 |
| 5 | BACKWARD FACING STEP FLOW | Author keyword | 5 | 34% | 1% | 11 |
| 6 | LMFTA | Address | 4 | 75% | 0% | 3 |
| 7 | SURFACE MOUNTED RIB | Author keyword | 4 | 75% | 0% | 3 |
| 8 | REATTACHMENT LENGTH | Author keyword | 4 | 36% | 1% | 9 |
| 9 | BLOCKED OFF METHOD | Author keyword | 3 | 57% | 0% | 4 |
| 10 | 3D BACKWARD FACING STEP | Author keyword | 3 | 100% | 0% | 3 |
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 | BACKWARD FACING STEP | 36 | 23% | 13% | 134 |
| 2 | REATTACHING FLOW | 22 | 58% | 3% | 25 |
| 3 | REATTACHMENT | 15 | 17% | 8% | 78 |
| 4 | TURBULENT SEPARATION BUBBLE | 13 | 58% | 2% | 15 |
| 5 | BLUFF RECTANGULAR PLATE | 12 | 86% | 1% | 6 |
| 6 | REATTACHING SHEAR LAYER | 9 | 83% | 1% | 5 |
| 7 | SURFACE MOUNTED OBSTACLE | 9 | 83% | 1% | 5 |
| 8 | TURBULENT SEPARATED FLOW | 8 | 75% | 1% | 6 |
| 9 | SHEAR LAYER | 7 | 10% | 6% | 61 |
| 10 | HIGHLY TURBULENT FLOWS | 6 | 80% | 0% | 4 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| A review of research on laminar mixed convection flow over backward- and forward-facing steps | 2003 | 50 | 13 | 100% |
| Aspects of turbulent boundary-layer separation | 1996 | 70 | 73 | 42% |
| TURBULENT BOUNDARY-LAYER SEPARATION | 1989 | 149 | 25 | 60% |
| Review: Diffuser design and performance analysis by a unified integral method - (Data bank contribution) | 1998 | 8 | 2 | 100% |
| Detection and measurement of the inverse axial flow by means of the flying hot wire technique | 2010 | 0 | 7 | 71% |
| Theories for base pressure in incompressible steady base flow | 1998 | 8 | 8 | 75% |
| PROGRESS IN TURBULENT FORCED-CONVECTION | 1988 | 7 | 51 | 27% |
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 | LMFTA | 4 | 75% | 0.3% | 3 |
| 2 | STROMUNGSMECH AERODYNAM | 3 | 42% | 0.5% | 5 |
| 3 | SEKRETARIAT HF 1 | 2 | 67% | 0.2% | 2 |
| 4 | HERMANN FOTTINGER STROMUNGSMECH | 2 | 21% | 0.8% | 8 |
| 5 | CSDF | 1 | 40% | 0.2% | 2 |
| 6 | INTH | 1 | 33% | 0.2% | 2 |
| 7 | ADV ENGN TESTING | 1 | 50% | 0.1% | 1 |
| 8 | DIE ENGN | 1 | 50% | 0.1% | 1 |
| 9 | ENGINEERS ARCHITECTS | 1 | 50% | 0.1% | 1 |
| 10 | ENSMA 6609 | 1 | 50% | 0.1% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000205426 | JEFFERY HAMEL PROBLEM//SUDDEN EXPANSION//DIVERGING CHANNEL |
| 2 | 0.0000177238 | SIDE DUMP COMBUSTOR//COMBUSTOR FLOW//JET IMPINGEMENTS |
| 3 | 0.0000129763 | TRANSPIRATION COOLING//UMR 5008 THERM LYON//COMPRESSIBLE OR INCOMPRESSIBLE FLUID |
| 4 | 0.0000125890 | OFFSET JET//PLANE WALL JET//WALL JET |
| 5 | 0.0000116727 | SECOND MOMENT CLOSURE//ELLIPTIC RELAXATION//TURBULENCE MODELLING |
| 6 | 0.0000112199 | SYNTHETIC JET//SYNTHETIC JETS//SYNTHETIC JET ACTUATOR |
| 7 | 0.0000096552 | TURBULENT BOUNDARY LAYERS//WALL TURBULENCE//TURBULENT BOUNDARY LAYER |
| 8 | 0.0000093681 | NUMERICAL HEAT TRANSFER PART B-FUNDAMENTALS//LECUSSO SCHEME//GENERAL CURVILINEAR CO ORDINATES |
| 9 | 0.0000091892 | FAR WAKE//TURBULENT WAKE//TURBULENT MIXING UNSTEADY AERODYNAM |
| 10 | 0.0000090839 | AE ACOUST VIBRAT//PROMOTING EXPERIENCES AERONAUT STRUCT ACOUS//WALL PRESSURE FLUCTUATIONS |