Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
20428 | 399 | 19.2 | 38% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
1422 | 7468 | INTERNATIONAL JOURNAL OF AEROACOUSTICS//AEROACOUSTICS//EXPERIMENTS IN FLUIDS |
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 | SHOCK VORTEX INTERACTION | Author keyword | 19 | 64% | 5% | 18 |
2 | BACKGROUND ORIENTED SCHLIEREN | Author keyword | 12 | 75% | 2% | 9 |
3 | COMPRESSIBLE VORTEX RING | Author keyword | 8 | 100% | 1% | 5 |
4 | BACKGROUND ORIENTED SCHLIEREN BOS | Author keyword | 6 | 100% | 1% | 4 |
5 | GAS DYNAM | Address | 3 | 29% | 3% | 10 |
6 | DENSITY SENSITIVE FLOW VISUALIZATION TECHNIQUES | Author keyword | 3 | 100% | 1% | 3 |
7 | MUZZLE BLAST WAVE | Author keyword | 2 | 67% | 1% | 2 |
8 | MUZZLE FLOW | Author keyword | 2 | 67% | 1% | 2 |
9 | SHOCK TUBE FLOWS | Author keyword | 2 | 67% | 1% | 2 |
10 | VORTEX SHOCK INTERACTION | Author keyword | 2 | 67% | 1% | 2 |
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 | BACKGROUND ORIENTED SCHLIEREN | 6 | 48% | 3% | 10 |
2 | BLAST FLOWFIELDS | 6 | 100% | 1% | 4 |
3 | MUZZLE BLAST | 4 | 46% | 2% | 6 |
4 | LOAD DEPOSIT REMOVAL | 3 | 100% | 1% | 3 |
5 | QUANTITATIVE SCHLIEREN | 3 | 100% | 1% | 3 |
6 | DIFFRACTING SHOCK WAVE | 3 | 60% | 1% | 3 |
7 | ORIENTED SCHLIEREN TECHNIQUE | 3 | 60% | 1% | 3 |
8 | BALLISTIC RANGE | 2 | 67% | 1% | 2 |
9 | CONVEX CORNER | 2 | 67% | 1% | 2 |
10 | OPEN ENDS | 2 | 50% | 1% | 3 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Half a century of continuous shock interaction investigations in the Joint Institute for High Temperatures of Russian Academy of Sciences | 2014 | 1 | 19 | 58% |
Dynamic structure of confined shocks undergoing sudden expansion | 2002 | 21 | 8 | 50% |
Filming the invisible - time-resolved visualization of compressible flows | 2010 | 4 | 21 | 48% |
Background-oriented schlieren (BOS) techniques | 2015 | 0 | 47 | 79% |
Impulse noise and its control | 1998 | 11 | 7 | 43% |
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 | GAS DYNAM | 3 | 29% | 2.5% | 10 |
2 | PENN STATE GAS DYNAM | 1 | 100% | 0.5% | 2 |
3 | MACE | 1 | 11% | 2.8% | 11 |
4 | FLOW UNIT | 1 | 22% | 1.0% | 4 |
5 | TRANSIENT PHYS | 1 | 10% | 1.8% | 7 |
6 | AERODYNAM STROMUNGSTECHN | 1 | 50% | 0.3% | 1 |
7 | ECOFRIENDLY HEAT COLD ENERGY MECH TEAM | 1 | 50% | 0.3% | 1 |
8 | ENGNKWANAK GU | 1 | 50% | 0.3% | 1 |
9 | MECH AEROSP ENGN SYST | 1 | 50% | 0.3% | 1 |
10 | MICRO IMAGING SYST | 1 | 50% | 0.3% | 1 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000236045 | VORTEX RING//VORTEX RINGS//POWER MACHINE BLDG |
2 | 0.0000170482 | GAS SUSPENSIONS//DETONATION SUPPRESSION//SHOCK FOAM INTERACTION |
3 | 0.0000133663 | HARTMANN WHISTLE//FLORIDA ADV AEROPROPULS//MACH DISK |
4 | 0.0000128396 | INFORMAT PHYS ENGN//MOIRE DEFLECTOMETRY//SANDWICH HOLOGRAPHY |
5 | 0.0000112328 | BALLIST CHINA//SPIN STABILIZED PROJECTILE//INTERIOR BALLISTICS |
6 | 0.0000106211 | TRANSONIC SHOCK//NONLINEAR WAVE SYSTEM//TRANSONIC SHOCKS |
7 | 0.0000089958 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
8 | 0.0000089878 | RESTRICTED SHOCK SEPARATION//FREE SHOCK SEPARATION//SIDE LOADS |
9 | 0.0000073619 | STRATIFIED TURBULENCE//STRATIFIED FLUID//OSCILLATIONS OF A CYLINDER |
10 | 0.0000071745 | INTERNATIONAL JOURNAL OF AEROACOUSTICS//COMPUTATIONAL AEROACOUSTICS//JET NOISE |