Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 25986 | 219 | 21.6 | 25% |
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 | BUFFET | Author keyword | 4 | 32% | 5% | 10 |
| 2 | AERODYNAM ENERGET MODELLING | Address | 1 | 31% | 2% | 4 |
| 3 | SHOCK BUFFET | Author keyword | 1 | 100% | 1% | 2 |
| 4 | SHOCK INDUCED OSCILLATIONS | Author keyword | 1 | 100% | 1% | 2 |
| 5 | TURBULENCE MODELLING PREDICT UNIT | Address | 1 | 100% | 1% | 2 |
| 6 | WALL INTERFERENCE | Author keyword | 1 | 33% | 1% | 2 |
| 7 | HWA | Address | 1 | 50% | 0% | 1 |
| 8 | ONERA M6 WING | Author keyword | 1 | 50% | 0% | 1 |
| 9 | SHOCK WAVE OSCILLATION | Author keyword | 1 | 50% | 0% | 1 |
| 10 | TRANSONIC BUFFET | Author keyword | 1 | 50% | 0% | 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 | BUFFET | 4 | 32% | 5% | 10 | Search BUFFET | Search BUFFET |
| 2 | SHOCK BUFFET | 1 | 100% | 1% | 2 | Search SHOCK+BUFFET | Search SHOCK+BUFFET |
| 3 | SHOCK INDUCED OSCILLATIONS | 1 | 100% | 1% | 2 | Search SHOCK+INDUCED+OSCILLATIONS | Search SHOCK+INDUCED+OSCILLATIONS |
| 4 | WALL INTERFERENCE | 1 | 33% | 1% | 2 | Search WALL+INTERFERENCE | Search WALL+INTERFERENCE |
| 5 | ONERA M6 WING | 1 | 50% | 0% | 1 | Search ONERA+M6+WING | Search ONERA+M6+WING |
| 6 | SHOCK WAVE OSCILLATION | 1 | 50% | 0% | 1 | Search SHOCK+WAVE+OSCILLATION | Search SHOCK+WAVE+OSCILLATION |
| 7 | TRANSONIC BUFFET | 1 | 50% | 0% | 1 | Search TRANSONIC+BUFFET | Search TRANSONIC+BUFFET |
| 8 | WIND TUNNEL CORRECTIONS | 1 | 50% | 0% | 1 | Search WIND+TUNNEL+CORRECTIONS | Search WIND+TUNNEL+CORRECTIONS |
| 9 | SUPERCRITICAL AIRFOIL | 1 | 18% | 1% | 3 | Search SUPERCRITICAL+AIRFOIL | Search SUPERCRITICAL+AIRFOIL |
| 10 | BUFFET ONSET | 0 | 33% | 0% | 1 | Search BUFFET+ONSET | Search BUFFET+ONSET |
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 | TRANSONIC BUFFET | 8 | 75% | 3% | 6 |
| 2 | SHOCK OSCILLATIONS | 8 | 100% | 2% | 5 |
| 3 | SUPERCRITICAL AIRFOIL | 6 | 48% | 5% | 10 |
| 4 | BUFFET | 2 | 32% | 3% | 6 |
| 5 | ORGANIZED MODES | 2 | 43% | 1% | 3 |
| 6 | SHOCK VORTEX INTERACTION | 1 | 33% | 1% | 3 |
| 7 | BODY POTENTIAL FLOW | 1 | 50% | 0% | 1 |
| 8 | EQUILIBRIUM BOUNDARY LAYERS | 1 | 50% | 0% | 1 |
| 9 | WALL TECHNOLOGY | 1 | 50% | 0% | 1 |
| 10 | BUFFETING FLOWS | 0 | 33% | 0% | 1 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| ADAPTIVE WALL TECHNOLOGY FOR IMPROVED WIND-TUNNEL TESTING TECHNIQUES - A REVIEW | 1995 | 11 | 3 | 100% |
| Self-sustained shock oscillations on airfoils at transonic speeds | 2001 | 47 | 19 | 58% |
| Update on progress in adaptive wind tunnel wall technology | 2004 | 6 | 5 | 100% |
| Aerodynamic scaling to free flight conditions: Past and present | 2008 | 5 | 6 | 33% |
| ADAPTIVE WIND TUNNELS | 1988 | 7 | 9 | 100% |
| Unsteady aerodynamics: retrospect and prospect | 1999 | 6 | 13 | 69% |
| Recent experience in improving the accuracy of wall interference corrections in TsAGI T-128 wind tunnel | 2001 | 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 | AERODYNAM ENERGET MODELLING | 1 | 31% | 1.8% | 4 |
| 2 | TURBULENCE MODELLING PREDICT UNIT | 1 | 100% | 0.9% | 2 |
| 3 | HWA | 1 | 50% | 0.5% | 1 |
| 4 | UNITE MIXTE RECH CNRS INPT UMR 5502 | 1 | 50% | 0.5% | 1 |
| 5 | AERODYNAM ENERGET MODELS | 0 | 20% | 0.9% | 2 |
| 6 | AERODYNAM ENERGET | 0 | 33% | 0.5% | 1 |
| 7 | AERO ASTRONAUT | 0 | 20% | 0.5% | 1 |
| 8 | FLUID MECH TOULOUSE | 0 | 20% | 0.5% | 1 |
| 9 | UMR5502 | 0 | 17% | 0.5% | 1 |
| 10 | TELFORD | 0 | 14% | 0.5% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000182697 | GURNEY FLAP//DYNAMIC STALL//OSCILLATING AIRFOIL |
| 2 | 0.0000123514 | GROUND EFFECT//WING IN GROUND EFFECT//POWER AUGMENTED RAM |
| 3 | 0.0000109500 | LOCAL SUPERSONIC REGIONS//INVERSE DESIGN//AEROSP PROP GRP |
| 4 | 0.0000103044 | CONFIGURAT AERODYNAM BRANCH//AVIAT PROGRAM GRP//CIVIL TRANSPORT TEAM |
| 5 | 0.0000098222 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
| 6 | 0.0000090693 | JOURNAL OF AIRCRAFT//AEROELASTICITY//FLUTTER |
| 7 | 0.0000076561 | MOMENTUM INJECTION//CLAUSER TECHNIQUE//DEEP WATER RISERS |
| 8 | 0.0000074212 | AV CONTROL//AVION CONTROL//ADAPTIVE WINGS |
| 9 | 0.0000062142 | WET STEAM//CASCADES OF BLADES//SUPERSONIC SEPARATOR |
| 10 | 0.0000060690 | DELTA WING//HIGH ANGLE OF ATTACK//DOUBLE DELTA WING |