Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 18623 | 477 | 21.0 | 28% |
Classes in level above (level 2) |
| ID, lev. above |
Publications | Label for level above |
|---|---|---|
| 1797 | 5767 | JOURNAL OF SPACECRAFT AND ROCKETS//HYPERSON//SCRAMJET |
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 | OPPOSING JET | Author keyword | 15 | 73% | 2% | 11 |
| 2 | HYPERSONIC SHOCK TUNNEL | Author keyword | 8 | 75% | 1% | 6 |
| 3 | FORWARD FACING CAVITY | Author keyword | 7 | 64% | 1% | 7 |
| 4 | IMPULSE FACILITY | Author keyword | 6 | 80% | 1% | 4 |
| 5 | ACCELEROMETER BALANCE | Author keyword | 6 | 100% | 1% | 4 |
| 6 | SHOCK TUNNEL | Author keyword | 5 | 29% | 3% | 16 |
| 7 | ACCELEROMETER FORCE BALANCE | Author keyword | 3 | 100% | 1% | 3 |
| 8 | HYPERSON SHOCK WAVE | Address | 3 | 100% | 1% | 3 |
| 9 | LARGE ANGLE BLUNT CONE | Author keyword | 3 | 100% | 1% | 3 |
| 10 | THERMAL PRODUCT | Author keyword | 3 | 100% | 1% | 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 | OPPOSING JET | 15 | 73% | 2% | 11 | Search OPPOSING+JET | Search OPPOSING+JET |
| 2 | HYPERSONIC SHOCK TUNNEL | 8 | 75% | 1% | 6 | Search HYPERSONIC+SHOCK+TUNNEL | Search HYPERSONIC+SHOCK+TUNNEL |
| 3 | FORWARD FACING CAVITY | 7 | 64% | 1% | 7 | Search FORWARD+FACING+CAVITY | Search FORWARD+FACING+CAVITY |
| 4 | IMPULSE FACILITY | 6 | 80% | 1% | 4 | Search IMPULSE+FACILITY | Search IMPULSE+FACILITY |
| 5 | ACCELEROMETER BALANCE | 6 | 100% | 1% | 4 | Search ACCELEROMETER+BALANCE | Search ACCELEROMETER+BALANCE |
| 6 | SHOCK TUNNEL | 5 | 29% | 3% | 16 | Search SHOCK+TUNNEL | Search SHOCK+TUNNEL |
| 7 | ACCELEROMETER FORCE BALANCE | 3 | 100% | 1% | 3 | Search ACCELEROMETER+FORCE+BALANCE | Search ACCELEROMETER+FORCE+BALANCE |
| 8 | LARGE ANGLE BLUNT CONE | 3 | 100% | 1% | 3 | Search LARGE+ANGLE+BLUNT+CONE | Search LARGE+ANGLE+BLUNT+CONE |
| 9 | THERMAL PRODUCT | 3 | 100% | 1% | 3 | Search THERMAL+PRODUCT | Search THERMAL+PRODUCT |
| 10 | RESONANT HOLOGRAPHIC INTERFEROMETRY | 2 | 67% | 0% | 2 | Search RESONANT+HOLOGRAPHIC+INTERFEROMETRY | Search RESONANT+HOLOGRAPHIC+INTERFEROMETRY |
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 | BODY FLOWS | 9 | 83% | 1% | 5 |
| 2 | MISSILE CONFIGURATIONS | 9 | 83% | 1% | 5 |
| 3 | LIQUID CONTACT | 8 | 75% | 1% | 6 |
| 4 | NOSE CAVITY | 8 | 100% | 1% | 5 |
| 5 | IMPULSE FACILITIES | 7 | 64% | 1% | 7 |
| 6 | DRIVING MECHANISMS | 7 | 67% | 1% | 6 |
| 7 | SURFACE JUNCTION THERMOCOUPLES | 6 | 80% | 1% | 4 |
| 8 | ANGLE BLUNT CONES | 6 | 100% | 1% | 4 |
| 9 | FORWARD FACING CAVITY | 6 | 100% | 1% | 4 |
| 10 | SUPERORBITAL EXPANSION TUBE | 6 | 100% | 1% | 4 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Recent advances in the aerothermodynamics of spiked hypersonic vehicles | 2011 | 9 | 28 | 86% |
| The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects | 1997 | 15 | 21 | 76% |
| Separation length in high-enthalpy shock/boundary-layer interaction | 2000 | 14 | 30 | 63% |
| Nonequilibrium recombination after a curved shock wave | 2010 | 1 | 4 | 75% |
| Optical imaging techniques for hypersonic impulse facilities | 2007 | 8 | 42 | 24% |
| A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations | 2015 | 0 | 57 | 67% |
| HYPER-VELOCITY AERODYNAMICS WITH CHEMICAL NONEQUILIBRIUM | 1989 | 19 | 3 | 67% |
| On vortex loops and filaments: three examples of numerical predictions of flows containing vortices | 2003 | 3 | 17 | 24% |
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 | HYPERSON SHOCK WAVE | 3 | 100% | 0.6% | 3 |
| 2 | HYPERSON | 2 | 14% | 2.9% | 14 |
| 3 | AEROENGINE TECHNOL | 1 | 40% | 0.4% | 2 |
| 4 | INTERDISCIPLINARY SHOCK WAVE | 1 | 17% | 0.8% | 4 |
| 5 | AEROSP PROP REACTING FLOWS UNIT | 1 | 50% | 0.2% | 1 |
| 6 | AEROTHERMAL TEST IL | 1 | 50% | 0.2% | 1 |
| 7 | CHOFU AEROSP | 1 | 50% | 0.2% | 1 |
| 8 | EXCELLENCE COMP SIMULAT | 1 | 50% | 0.2% | 1 |
| 9 | FLIGHT PROPULS | 1 | 50% | 0.2% | 1 |
| 10 | HIGH TEMP DYNAM | 1 | 50% | 0.2% | 1 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000193639 | SCRAMJET//SUPERSONIC COMBUSTION//JOURNAL OF PROPULSION AND POWER |
| 2 | 0.0000144484 | AEROTHERMODYNAM BRANCH//JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER//REACTING FLOW ENVIRONM BRANCH |
| 3 | 0.0000128405 | HEAT FLUX GAGE//MICRO C OUEST//NON INTEGER SYSTEM IDENTIFICATION |
| 4 | 0.0000128027 | MECHANICAL Q SWITCHING//REPETITIVELY PULSED LASING//OPTICAL PULSATING DISCHARGE |
| 5 | 0.0000100759 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
| 6 | 0.0000099351 | GEODETIC COORDINATES//ELLIPSOIDAL NORMAL//MULTI HOLE PRESSURE PROBE |
| 7 | 0.0000081747 | ENGINE THERMAL MANAGEMENT//AIR COOLED ENGINE//INSTANTANEOUS HEAT FLUX |
| 8 | 0.0000067843 | OPERATOR DIFFERENCE SCHEMES//FINITE VOLUME TIME DOMAIN//CYLINDRICAL HOUSING |
| 9 | 0.0000066948 | SETTLING CHAMBER//SCI SYST ANAL//CHLORINE TRIFLUORIDE OXIDE |
| 10 | 0.0000061748 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |