Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
7475 | 1283 | 22.7 | 32% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
1291 | 8190 | VORTEX INDUCED VIBRATIONS//VORTEX SHEDDING//JOURNAL OF FLUIDS AND STRUCTURES |
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 | DELTA WING | Author keyword | 22 | 44% | 3% | 39 |
2 | HIGH ANGLE OF ATTACK | Author keyword | 7 | 32% | 1% | 19 |
3 | DOUBLE DELTA WING | Author keyword | 6 | 80% | 0% | 4 |
4 | ASYMMETRIC VORTEX | Author keyword | 6 | 58% | 1% | 7 |
5 | FLIGHT PHYS LOADS | Address | 6 | 53% | 1% | 8 |
6 | WING ROCK | Author keyword | 6 | 47% | 1% | 9 |
7 | X 31 | Author keyword | 6 | 100% | 0% | 4 |
8 | AEROSP VEHICLES | Address | 4 | 42% | 1% | 8 |
9 | ROKETSAN | Address | 4 | 75% | 0% | 3 |
10 | UNCERTAINTY AND DISTURBANCE ESTIMATION | Author keyword | 4 | 75% | 0% | 3 |
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 | DELTA WING | 22 | 44% | 3% | 39 | Search DELTA+WING | Search DELTA+WING |
2 | HIGH ANGLE OF ATTACK | 7 | 32% | 1% | 19 | Search HIGH+ANGLE+OF+ATTACK | Search HIGH+ANGLE+OF+ATTACK |
3 | DOUBLE DELTA WING | 6 | 80% | 0% | 4 | Search DOUBLE+DELTA+WING | Search DOUBLE+DELTA+WING |
4 | ASYMMETRIC VORTEX | 6 | 58% | 1% | 7 | Search ASYMMETRIC+VORTEX | Search ASYMMETRIC+VORTEX |
5 | WING ROCK | 6 | 47% | 1% | 9 | Search WING+ROCK | Search WING+ROCK |
6 | X 31 | 6 | 100% | 0% | 4 | Search X+31 | Search X+31 |
7 | UNCERTAINTY AND DISTURBANCE ESTIMATION | 4 | 75% | 0% | 3 | Search UNCERTAINTY+AND+DISTURBANCE+ESTIMATION | Search UNCERTAINTY+AND+DISTURBANCE+ESTIMATION |
8 | HIGH ANGLE OF ATTACK AERODYNAMICS | 3 | 43% | 0% | 6 | Search HIGH+ANGLE+OF+ATTACK+AERODYNAMICS | Search HIGH+ANGLE+OF+ATTACK+AERODYNAMICS |
9 | TIP PERTURBATION | 3 | 100% | 0% | 3 | Search TIP+PERTURBATION | Search TIP+PERTURBATION |
10 | UNCERTAINTY AND DISTURBANCE ESTIMATOR UDE | 3 | 45% | 0% | 5 | Search UNCERTAINTY+AND+DISTURBANCE+ESTIMATOR+UDE | Search UNCERTAINTY+AND+DISTURBANCE+ESTIMATOR+UDE |
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 | VORTEX ASYMMETRY | 64 | 100% | 2% | 21 |
2 | DELTA WINGS | 46 | 70% | 3% | 38 |
3 | OGIVE CYLINDER | 33 | 100% | 1% | 13 |
4 | SLENDER DELTA WINGS | 27 | 60% | 2% | 29 |
5 | ASYMMETRIC VORTICES | 20 | 100% | 1% | 9 |
6 | SUPPORT INTERFERENCE | 11 | 100% | 0% | 6 |
7 | DISCRETE VORTICES | 9 | 64% | 1% | 9 |
8 | STREAMWISE VORTEX | 9 | 67% | 1% | 8 |
9 | NONSLENDER DELTA WINGS | 8 | 62% | 1% | 8 |
10 | FOREBODY | 6 | 80% | 0% | 4 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Unsteady aerodynamics of nonslender delta wings | 2005 | 61 | 35 | 83% |
Review of flow control mechanisms of leading-edge vortices | 2007 | 19 | 36 | 89% |
Robert Legendre and Henri Werle: Toward the elucidation of three-dimensional separation | 2001 | 49 | 4 | 100% |
Research into vortex breakdown control | 2001 | 46 | 19 | 100% |
Wing/vortex interactions and wing rock | 1999 | 31 | 52 | 92% |
Review of unsteady vortex flows over slender delta wings | 2005 | 33 | 79 | 87% |
The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers | 2003 | 32 | 27 | 81% |
Unsteady flow phenomena associated with leading-edge vortices | 2008 | 10 | 9 | 100% |
A review of the Magnus effect in aeronautics | 2012 | 7 | 11 | 45% |
Toward a theoretical description of vortex wake asymmetry | 2010 | 4 | 13 | 77% |
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 | FLIGHT PHYS LOADS | 6 | 53% | 0.6% | 8 |
2 | AEROSP VEHICLES | 4 | 42% | 0.6% | 8 |
3 | ROKETSAN | 4 | 75% | 0.2% | 3 |
4 | SEEK EAGLE OFF | 2 | 36% | 0.4% | 5 |
5 | AERONAUT SYST PROGRAM | 2 | 67% | 0.2% | 2 |
6 | ADV AIRCRAFT TECHNOL | 1 | 100% | 0.2% | 2 |
7 | AIRCRAFT AERODYNAM GRP | 1 | 100% | 0.2% | 2 |
8 | PACKARD 354 | 1 | 19% | 0.5% | 6 |
9 | CONFIGURAT AERODYNAM BRANCH | 1 | 16% | 0.5% | 7 |
10 | AIR SYST COMMAND | 1 | 11% | 0.7% | 9 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000131987 | GURNEY FLAP//DYNAMIC STALL//OSCILLATING AIRFOIL |
2 | 0.0000120559 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
3 | 0.0000099410 | MOMENTUM INJECTION//CLAUSER TECHNIQUE//DEEP WATER RISERS |
4 | 0.0000090940 | DYNAM SYST CONTROL BRANCH//AIRCRAFT PARAMETER ESTIMATION//FLIGHT DYNAM BRANCH |
5 | 0.0000088881 | AERODYNAM BRANCH//CONING MOTION//MISSILE SYST DAHLGREN |
6 | 0.0000079272 | THREE DIMENSIONAL TURBULENT BOUNDARY LAYER//MEAN THREE DIMENSIONALITY//PUMP JET |
7 | 0.0000078394 | TURBO MACHINERY//COMPOUND CHOKING//COMPOUND WAVES |
8 | 0.0000074021 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
9 | 0.0000073358 | CONTROL ALLOCATION//CONTROL OF UAVS//DIRECT ALLOCATION |
10 | 0.0000072067 | VORTEX BREAKDOWN//COMPOUND VORTEX//SWIRLING JET |