Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
5927 | 1487 | 26.7 | 36% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
2123 | 4634 | TRANSITION TO TURBULENCE//BOUNDARY LAYER STABILITY//BOUNDARY LAYER RECEPTIVITY |
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 | BOUNDARY LAYER STABILITY | Author keyword | 23 | 41% | 3% | 44 |
2 | LAMINAR TURBULENT TRANSITION | Author keyword | 15 | 28% | 3% | 45 |
3 | AEROMECH FLIGHT ENGN | Address | 15 | 71% | 1% | 12 |
4 | BOUNDARY LAYER RECEPTIVITY | Author keyword | 14 | 57% | 1% | 17 |
5 | ROTATING DISK FLOW | Author keyword | 12 | 44% | 1% | 20 |
6 | LAMINAR FLOW CONTROL | Author keyword | 9 | 64% | 1% | 9 |
7 | COMPRESSIBLE BOUNDARY LAYERS | Author keyword | 9 | 40% | 1% | 18 |
8 | CROSS FLOW INSTABILITY | Author keyword | 8 | 60% | 1% | 9 |
9 | SWEPT WING | Author keyword | 6 | 40% | 1% | 12 |
10 | COMPRESSIBLE BOUNDARY LAYER | Author keyword | 6 | 53% | 1% | 8 |
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 | TOLLMIEN SCHLICHTING WAVES | 42 | 48% | 4% | 64 |
2 | ATTACHMENT LINE | 42 | 94% | 1% | 15 |
3 | STATIONARY MODES | 41 | 90% | 1% | 18 |
4 | BOUNDARY LAYER TRANSITION | 32 | 36% | 5% | 73 |
5 | 3 DIMENSIONAL BOUNDARY LAYERS | 28 | 57% | 2% | 34 |
6 | FREE STREAM DISTURBANCES | 27 | 78% | 1% | 18 |
7 | LEADING EDGE RECEPTIVITY | 27 | 83% | 1% | 15 |
8 | CROSS FLOW VORTICES | 21 | 71% | 1% | 17 |
9 | BOUNDARY LAYER RECEPTIVITY | 19 | 63% | 1% | 19 |
10 | PARABOLIZED STABILITY EQUATIONS | 19 | 63% | 1% | 19 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Transition and Stability of High-Speed Boundary Layers | 2011 | 31 | 29 | 100% |
Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers | 2012 | 14 | 98 | 71% |
Parabolized stability equations | 1997 | 152 | 23 | 61% |
Stability and transition of three-dimensional boundary layers | 2003 | 128 | 43 | 95% |
Hypersonic laminar-turbulent transition on circular cones and scrarajet forebodies | 2004 | 62 | 54 | 67% |
Boundary-layer receptivity to freestream disturbances | 2002 | 120 | 43 | 65% |
Aircraft laminar flow control | 1998 | 92 | 8 | 88% |
PHYSICAL-MECHANISMS OF LAMINAR-BOUNDARY-LAYER TRANSITION | 1994 | 189 | 36 | 53% |
Modal Stability Theory | 2014 | 2 | 49 | 59% |
Effects of high-speed tunnel noise on laminar-turbulent transition | 2001 | 50 | 27 | 89% |
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 | AEROMECH FLIGHT ENGN | 15 | 71% | 0.8% | 12 |
2 | HYPERSON FLOW | 4 | 75% | 0.2% | 3 |
3 | AERODYNAM GASDYNAM | 3 | 16% | 1.3% | 20 |
4 | AEROTHERMAL AEROOPT EVALUAT | 3 | 100% | 0.2% | 3 |
5 | AEROTHERMODYNAM BRANCH | 3 | 15% | 1.1% | 17 |
6 | AFRL RQHV | 2 | 67% | 0.1% | 2 |
7 | TACT AIRCRAFT SYST | 2 | 67% | 0.1% | 2 |
8 | AERODYNAM GAS DYNAM | 2 | 19% | 0.5% | 8 |
9 | STATE TURBULENCE | 1 | 16% | 0.5% | 8 |
10 | AEROMECH AIRCRAFT ENGN | 1 | 100% | 0.1% | 2 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000275304 | GORTLER VORTICES//GOERTLER VORTICES//GORTLER INSTABILITY |
2 | 0.0000237446 | TRANSITION TO TURBULENCE//LINNE FLOW//ALGEBRAIC INSTABILITY |
3 | 0.0000198472 | TRIPLE DECK//TRIPLE DECK THEORY//UNSTEADY SEPARATION |
4 | 0.0000106719 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//LAMINAR SEPARATION BUBBLE//SEPARATED FLOW TRANSITION |
5 | 0.0000099468 | CONCENTRATION DIFFUSION EQUATION//TRIADIC RESONANCE//ORR SOMMERFELD |
6 | 0.0000089905 | SINGLE MODE FLUTTER//PLATE FLUTTER//COLLAPSIBLE TUBE |
7 | 0.0000080040 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
8 | 0.0000073942 | ROTOR STATOR CAVITY//ROTOR STATOR SYSTEM//THERMOFLUID SYST UTC |
9 | 0.0000066983 | VIS NAT COMPUTAT GRP//LONGITUDINAL LIBRATIONS//BILATERAL BOUNDS |
10 | 0.0000056678 | RIGA PLATE//SCI TECHNOL TRANSIENT PHYS//ELECTROMAGNETIC FLOW CONTROL |