Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
1980 | 2334 | 30.6 | 51% |
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 | TURBULENT BOUNDARY LAYERS | Author keyword | 117 | 57% | 6% | 137 |
2 | WALL TURBULENCE | Author keyword | 43 | 58% | 2% | 49 |
3 | TURBULENT BOUNDARY LAYER | Author keyword | 31 | 26% | 4% | 102 |
4 | RIBLETS | Author keyword | 29 | 61% | 1% | 31 |
5 | BOUNDARY LAYER STRUCTURE | Author keyword | 17 | 38% | 2% | 36 |
6 | OPPOSITION CONTROL | Author keyword | 14 | 100% | 0% | 7 |
7 | ADVERSE PRESSURE GRADIENT | Author keyword | 13 | 42% | 1% | 24 |
8 | DRAG REDUCTION | Author keyword | 12 | 11% | 5% | 107 |
9 | TURBULENCE CONTROL | Author keyword | 12 | 38% | 1% | 25 |
10 | INCOMPRESSIBLE TURBULENT BOUNDARY LAYER | Author keyword | 11 | 100% | 0% | 6 |
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 | TURBULENT BOUNDARY LAYERS | 117 | 57% | 6% | 137 | Search TURBULENT+BOUNDARY+LAYERS | Search TURBULENT+BOUNDARY+LAYERS |
2 | WALL TURBULENCE | 43 | 58% | 2% | 49 | Search WALL+TURBULENCE | Search WALL+TURBULENCE |
3 | TURBULENT BOUNDARY LAYER | 31 | 26% | 4% | 102 | Search TURBULENT+BOUNDARY+LAYER | Search TURBULENT+BOUNDARY+LAYER |
4 | RIBLETS | 29 | 61% | 1% | 31 | Search RIBLETS | Search RIBLETS |
5 | BOUNDARY LAYER STRUCTURE | 17 | 38% | 2% | 36 | Search BOUNDARY+LAYER+STRUCTURE | Search BOUNDARY+LAYER+STRUCTURE |
6 | OPPOSITION CONTROL | 14 | 100% | 0% | 7 | Search OPPOSITION+CONTROL | Search OPPOSITION+CONTROL |
7 | ADVERSE PRESSURE GRADIENT | 13 | 42% | 1% | 24 | Search ADVERSE+PRESSURE+GRADIENT | Search ADVERSE+PRESSURE+GRADIENT |
8 | DRAG REDUCTION | 12 | 11% | 5% | 107 | Search DRAG+REDUCTION | Search DRAG+REDUCTION |
9 | TURBULENCE CONTROL | 12 | 38% | 1% | 25 | Search TURBULENCE+CONTROL | Search TURBULENCE+CONTROL |
10 | INCOMPRESSIBLE TURBULENT BOUNDARY LAYER | 11 | 100% | 0% | 6 | Search INCOMPRESSIBLE+TURBULENT+BOUNDARY+LAYER | Search INCOMPRESSIBLE+TURBULENT+BOUNDARY+LAYER |
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 | CHANNEL FLOW | 99 | 18% | 21% | 498 |
2 | LOGARITHMIC REGION | 90 | 88% | 2% | 43 |
3 | VORTEX PACKETS | 80 | 84% | 2% | 43 |
4 | WALL TURBULENCE | 71 | 40% | 6% | 140 |
5 | OVERLAP REGION | 65 | 95% | 1% | 21 |
6 | NEAR WALL TURBULENCE | 64 | 37% | 6% | 138 |
7 | ATTACHED EDDY HYPOTHESIS | 48 | 100% | 1% | 17 |
8 | VISCOUS SUBLAYER | 45 | 56% | 2% | 55 |
9 | LARGE SCALE MOTIONS | 37 | 59% | 2% | 41 |
10 | SMOOTH WALL | 35 | 59% | 2% | 39 |
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 TURBULENCE | 9 | 11% | 3% | 79 |
Reviews |
Title | Publ. year | Cit. | Active references | % act. ref. to same field |
---|---|---|---|---|
RECENT PROGRESS IN EXPLORING DRAG REDUCTION MECHANISM OF REAL SHARKSKIN SURFACE: A REVIEW | 2015 | 4 | 36 | 69% |
High-Reynolds Number Wall Turbulence | 2011 | 103 | 103 | 93% |
Turbulent flows over rough walls | 2004 | 338 | 52 | 73% |
Cascades in Wall-Bounded Turbulence | 2012 | 33 | 55 | 89% |
COHERENT MOTIONS IN THE TURBULENT BOUNDARY-LAYER | 1991 | 1056 | 42 | 71% |
Incompressible zero-pressure-gradient turbulent boundary layer: An assessment of the data | 1996 | 157 | 32 | 75% |
Drag reduction in turbulent boundary layers by in-plane wall motion | 2011 | 19 | 29 | 86% |
Shark-skin surfaces for fluid-drag reduction in turbulent flow: a review | 2010 | 50 | 24 | 58% |
Advanced progresses in nature gas pipelining applying different drag reduction/energy saving technologies: a review | 2015 | 1 | 42 | 36% |
Aircraft viscous drag reduction using riblets | 2002 | 48 | 20 | 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 | MECH THERMO FLUID DYNAM | 8 | 70% | 0.3% | 7 |
2 | WALTER BASSETT AERODYNAM | 8 | 70% | 0.3% | 7 |
3 | MECHANOPHYS | 6 | 80% | 0.2% | 4 |
4 | TURBULENCE COMPLEX FLOW | 6 | 50% | 0.4% | 9 |
5 | LINNE FLOW | 6 | 12% | 1.9% | 45 |
6 | EXPT AEROGASDYNAM | 6 | 100% | 0.2% | 4 |
7 | DISCIPLINE MECH ENGN | 3 | 16% | 0.8% | 19 |
8 | CSDF | 3 | 60% | 0.1% | 3 |
9 | HEAT VACUUM | 2 | 67% | 0.1% | 2 |
10 | PHYS FLUID DYNAM | 2 | 27% | 0.3% | 7 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000214046 | RIGA PLATE//SCI TECHNOL TRANSIENT PHYS//ELECTROMAGNETIC FLOW CONTROL |
2 | 0.0000161697 | FAR WAKE//TURBULENT WAKE//TURBULENT MIXING UNSTEADY AERODYNAM |
3 | 0.0000141504 | TRANSITION TO TURBULENCE//LINNE FLOW//ALGEBRAIC INSTABILITY |
4 | 0.0000127910 | LARGE EDDY SIMULATION//SUBGRID SCALE MODEL//THEORET SECT |
5 | 0.0000119698 | AE ACOUST VIBRAT//PROMOTING EXPERIENCES AERONAUT STRUCT ACOUS//WALL PRESSURE FLUCTUATIONS |
6 | 0.0000118159 | SECOND MOMENT CLOSURE//ELLIPTIC RELAXATION//TURBULENCE MODELLING |
7 | 0.0000110568 | THREE DIMENSIONAL TURBULENT BOUNDARY LAYER//MEAN THREE DIMENSIONALITY//PUMP JET |
8 | 0.0000096552 | BACKWARD FACING STEP//FORWARD FACING STEP//SEPARATED AND REATTACHED FLOW |
9 | 0.0000095313 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//LAMINAR SEPARATION BUBBLE//SEPARATED FLOW TRANSITION |
10 | 0.0000084349 | MICROBREAKING//SURFACE JETS//SUBGRID SCALE SGS MODEL |