Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
34130 | 78 | 23.6 | 18% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
1273 | 8321 | JOURNAL OF THE AMERICAN HELICOPTER SOCIETY//JOURNAL OF AIRCRAFT//VERTICA |
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 | TURBO MACHINERY | Address | 2 | 50% | 4% | 3 |
2 | COMPOUND CHOKING | Author keyword | 1 | 100% | 3% | 2 |
3 | COMPOUND WAVES | Author keyword | 1 | 50% | 1% | 1 |
4 | CONTRAVARIANT VELOCITY | Author keyword | 0 | 33% | 1% | 1 |
5 | PERFORMANCE CONTROL SYST | Address | 0 | 33% | 1% | 1 |
6 | MINIMUM TIME TRAJECTORIES | Author keyword | 0 | 25% | 1% | 1 |
7 | SMAC METHOD | Author keyword | 0 | 14% | 1% | 1 |
8 | AERODYNAM ENERGET PORPULS | Address | 0 | 100% | 1% | 1 |
9 | BOMBERS AS JS UCAVS | Author keyword | 0 | 100% | 1% | 1 |
10 | COMPOUND SOUND WAVE | Author keyword | 0 | 100% | 1% | 1 |
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 | COMPOUND CHOKING | 1 | 100% | 3% | 2 | Search COMPOUND+CHOKING | Search COMPOUND+CHOKING |
2 | COMPOUND WAVES | 1 | 50% | 1% | 1 | Search COMPOUND+WAVES | Search COMPOUND+WAVES |
3 | CONTRAVARIANT VELOCITY | 0 | 33% | 1% | 1 | Search CONTRAVARIANT+VELOCITY | Search CONTRAVARIANT+VELOCITY |
4 | MINIMUM TIME TRAJECTORIES | 0 | 25% | 1% | 1 | Search MINIMUM+TIME+TRAJECTORIES | Search MINIMUM+TIME+TRAJECTORIES |
5 | SMAC METHOD | 0 | 14% | 1% | 1 | Search SMAC+METHOD | Search SMAC+METHOD |
6 | BOMBERS AS JS UCAVS | 0 | 100% | 1% | 1 | Search BOMBERS+AS+JS+UCAVS | Search BOMBERS+AS+JS+UCAVS |
7 | COMPOUND SOUND WAVE | 0 | 100% | 1% | 1 | Search COMPOUND+SOUND+WAVE | Search COMPOUND+SOUND+WAVE |
8 | DUAL SUBSONIC STREAMS | 0 | 100% | 1% | 1 | Search DUAL+SUBSONIC+STREAMS | Search DUAL+SUBSONIC+STREAMS |
9 | F 22 | 0 | 100% | 1% | 1 | Search F+22 | Search F+22 |
10 | F135 F136 ADVENT PROPULSION | 0 | 100% | 1% | 1 | Search F135++F136++ADVENT+PROPULSION | Search F135++F136++ADVENT+PROPULSION |
Key Words Plus |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
THRUST VECTORING FOR FLIGHT CONTROL AND SAFETY - A REVIEW | 1994 | 5 | 10 | 90% |
The New Era of Stealth, Tailless, Vectored Aircraft. A 2010 Review on Current & Future Designs and Applications of Manned and Unmanned, Super-Agile and Safest Military v. Civil Jets | 2010 | 0 | 8 | 100% |
A NAVIER STOKES CODE FOR S-SHAPED DIFFUSERS - A REVIEW | 1988 | 0 | 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 | TURBO MACHINERY | 2 | 50% | 3.8% | 3 |
2 | PERFORMANCE CONTROL SYST | 0 | 33% | 1.3% | 1 |
3 | AERODYNAM ENERGET PORPULS | 0 | 100% | 1.3% | 1 |
4 | FLIGHT MECH PROP | 0 | 100% | 1.3% | 1 |
5 | GAS TURBINE JET ENGINE | 0 | 100% | 1.3% | 1 |
6 | GAS TURBINE JET ENGINES | 0 | 100% | 1.3% | 1 |
7 | JET ENGINE | 0 | 100% | 1.3% | 1 |
8 | PLATFORMS LAUNCHERS | 0 | 100% | 1.3% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000205112 | INVERSE SIMULATION//FLIGHT DYNAMICS MODELING//PROPELLER DRIVEN AIRPLANE |
2 | 0.0000133887 | CONTROL ALLOCATION//CONTROL OF UAVS//DIRECT ALLOCATION |
3 | 0.0000120226 | TRAPPED VORTEX COMBUSTOR//TRAPPED VORTEX//SCI TECHNOL AEROENGINES AEROTHERMO |
4 | 0.0000109550 | LEARNING CLASSIFIER SYSTEMS//XCS//ILLIGAL |
5 | 0.0000100234 | GAS WIPING//GAS JET WIPING//AIR KNIFE |
6 | 0.0000100216 | WINDSHEAR PROBLEMS//ABORT LANDING//WIND IDENTIFICATION |
7 | 0.0000093418 | GURNEY FLAP//DYNAMIC STALL//OSCILLATING AIRFOIL |
8 | 0.0000090341 | HARTMANN WHISTLE//FLORIDA ADV AEROPROPULS//MACH DISK |
9 | 0.0000078394 | DELTA WING//HIGH ANGLE OF ATTACK//DOUBLE DELTA WING |
10 | 0.0000072571 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |