Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
31416 | 153 | 20.0 | 26% |
Hierarchy of classes |
The table includes all classes above and classes immediately below the current class. |
Cluster id | Level | Cluster label | #P |
---|---|---|---|
18 | 4 | THERMODYNAMICS//ENERGY & FUELS//ENGINEERING, CHEMICAL | 531182 |
68 | 3 | ENGINEERING, AEROSPACE//AIAA JOURNAL//MECHANICS | 84081 |
1263 | 2 | ENGINEERING, AEROSPACE//JOURNAL OF SPACECRAFT AND ROCKETS//JOURNAL OF PROPULSION AND POWER | 8803 |
31416 | 1 | FREE PISTON DRIVER//TUNED OPERATION//IMPULSE FACILITY | 153 |
Terms with highest relevance score |
rank | Term | termType | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|---|
1 | FREE PISTON DRIVER | authKW | 997893 | 3% | 100% | 5 |
2 | TUNED OPERATION | authKW | 997893 | 3% | 100% | 5 |
3 | IMPULSE FACILITY | authKW | 831576 | 3% | 83% | 5 |
4 | EXPANSION TUBE | authKW | 580582 | 5% | 36% | 8 |
5 | FREE PISTON SHOCK TUNNEL | authKW | 449050 | 2% | 75% | 3 |
6 | DIAPHRAGMLESS | authKW | 399157 | 1% | 100% | 2 |
7 | MICRO SHOCK WAVE | authKW | 399157 | 1% | 100% | 2 |
8 | STALKER TUBE | authKW | 399157 | 1% | 100% | 2 |
9 | DETONATION DRIVER | authKW | 359239 | 2% | 60% | 3 |
10 | RESONANT HOLOGRAPHIC INTERFEROMETRY | authKW | 266103 | 1% | 67% | 2 |
Web of Science journal categories |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | Engineering, Aerospace | 8270 | 35% | 0% | 54 |
2 | Mechanics | 1340 | 33% | 0% | 50 |
3 | Physics, Fluids & Plasmas | 115 | 7% | 0% | 11 |
4 | Optics | 37 | 8% | 0% | 12 |
5 | Engineering, Mechanical | 28 | 5% | 0% | 8 |
6 | Instruments & Instrumentation | 15 | 4% | 0% | 6 |
7 | Mathematics, Applied | 6 | 4% | 0% | 6 |
8 | Thermodynamics | 4 | 2% | 0% | 3 |
9 | Computer Science, Interdisciplinary Applications | 3 | 2% | 0% | 3 |
10 | Physics, Multidisciplinary | 3 | 4% | 0% | 6 |
Address terms |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | AEROSCI SECT | 199579 | 1% | 100% | 1 |
2 | ALDIR | 199579 | 1% | 100% | 1 |
3 | FORUM EUROPEAN AUSTRALIAN SCI TECHNOL COOPERAT | 199579 | 1% | 100% | 1 |
4 | KAKUDA KIMIGAYA | 199579 | 1% | 100% | 1 |
5 | MACHINERY SPACE SYST | 199579 | 1% | 100% | 1 |
6 | MULTIDISCIPLINE OPTIMIZAT | 199579 | 1% | 100% | 1 |
7 | SHOCKWAVES HYPERSON | 199579 | 1% | 100% | 1 |
8 | TURBOMACHINERY GEN MACHINERY | 199579 | 1% | 100% | 1 |
9 | WIND TUNNEL MKT | 199579 | 1% | 100% | 1 |
10 | HYPERSON | 108231 | 5% | 7% | 8 |
Journals |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
---|---|---|---|---|---|
1 | SHOCK WAVES | 157842 | 19% | 3% | 29 |
2 | AIAA JOURNAL | 15629 | 20% | 0% | 30 |
3 | AERONAUTICAL JOURNAL | 4600 | 4% | 0% | 6 |
4 | AERONAUTICAL QUARTERLY | 3439 | 1% | 2% | 1 |
5 | JOURNAL OF SPACECRAFT AND ROCKETS | 3006 | 5% | 0% | 8 |
6 | JOURNAL OF THE INDIAN INSTITUTE OF SCIENCE | 1621 | 1% | 1% | 1 |
7 | AEROSPACE SCIENCE AND TECHNOLOGY | 1532 | 3% | 0% | 4 |
8 | USSR COMPUTATIONAL MATHEMATICS AND MATHEMATICAL PHYSICS | 1065 | 1% | 0% | 2 |
9 | SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS | 885 | 1% | 0% | 1 |
10 | EXPERIMENTS IN FLUIDS | 672 | 3% | 0% | 4 |
Author Key Words |
Rank | Term | Chi square | Shr. of publ. in class containing term |
Class's shr. of term's tot. occurrences |
#P with term in class |
LCSH search | Wikipedia search |
---|---|---|---|---|---|---|---|
1 | FREE PISTON DRIVER | 997893 | 3% | 100% | 5 | Search FREE+PISTON+DRIVER | Search FREE+PISTON+DRIVER |
2 | TUNED OPERATION | 997893 | 3% | 100% | 5 | Search TUNED+OPERATION | Search TUNED+OPERATION |
3 | IMPULSE FACILITY | 831576 | 3% | 83% | 5 | Search IMPULSE+FACILITY | Search IMPULSE+FACILITY |
4 | EXPANSION TUBE | 580582 | 5% | 36% | 8 | Search EXPANSION+TUBE | Search EXPANSION+TUBE |
5 | FREE PISTON SHOCK TUNNEL | 449050 | 2% | 75% | 3 | Search FREE+PISTON+SHOCK+TUNNEL | Search FREE+PISTON+SHOCK+TUNNEL |
6 | DIAPHRAGMLESS | 399157 | 1% | 100% | 2 | Search DIAPHRAGMLESS | Search DIAPHRAGMLESS |
7 | MICRO SHOCK WAVE | 399157 | 1% | 100% | 2 | Search MICRO+SHOCK+WAVE | Search MICRO+SHOCK+WAVE |
8 | STALKER TUBE | 399157 | 1% | 100% | 2 | Search STALKER+TUBE | Search STALKER+TUBE |
9 | DETONATION DRIVER | 359239 | 2% | 60% | 3 | Search DETONATION+DRIVER | Search DETONATION+DRIVER |
10 | RESONANT HOLOGRAPHIC INTERFEROMETRY | 266103 | 1% | 67% | 2 | Search RESONANT+HOLOGRAPHIC+INTERFEROMETRY | Search RESONANT+HOLOGRAPHIC+INTERFEROMETRY |
Core articles |
The table includes core articles in the class. The following variables is taken into account for the relevance score of an article in a cluster c: (1) Number of references referring to publications in the class. (2) Share of total number of active references referring to publications in the class. (3) Age of the article. New articles get higher score than old articles. (4) Citation rate, normalized to year. |
Rank | Reference | # ref. in cl. |
Shr. of ref. in cl. |
Citations |
---|---|---|---|---|
1 | JIANG, ZL , WU, B , GAO, YL , ZHAO, W , HU, ZM , (2015) DEVELOPMENT OF THE DETONATION-DRIVEN EXPANSION TUBE FOR ORBITAL SPEED EXPERIMENTS.SCIENCE CHINA-TECHNOLOGICAL SCIENCES. VOL. 58. ISSUE 4. P. 695 -700 | 6 | 100% | 0 |
2 | FENG, S , CHANG, JT , YANG, QC , BAO, W , (2016) SIMULATION STUDY ON MODELING FOR DESIGN PARAMETERS ANALYSIS OF FREE-PISTON TUNNELS.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. VOL. 230. ISSUE 12. P. 2330 -2342 | 5 | 100% | 0 |
3 | ABUL-HUDA, YM , GAMBA, M , (2016) TEST-MODEL-INDUCED INTERFERENCE EFFECTS IN EXPANSION TUBE FLOWS.AIAA JOURNAL. VOL. 54. ISSUE 7. P. 2171 -2178 | 8 | 57% | 0 |
4 | HRUSCHKA, R , O'BYRNE, S , KLEINE, H , (2008) DIODE-LASER-BASED NEAR-RESONANTLY ENHANCED FLOW VISUALIZATION IN SHOCK TUNNELS.APPLIED OPTICS. VOL. 47. ISSUE 24. P. 4352 -4360 | 5 | 100% | 2 |
5 | MCINTYRE, TJ , BISHOP, AI , EICHMANN, TN , RUBINSZTEIN-DUNLOP, H , (2003) ENHANCED FLOW VISUALIZATION WITH NEAR-RESONANT HOLOGRAPHIC INTERFEROMETRY.APPLIED OPTICS. VOL. 42. ISSUE 22. P. 4445 -4451 | 7 | 78% | 8 |
6 | PARZIALE, NJ , RABINOVITCH, J , BLANQUART, G , HORNUNG, HG , SHEPHERD, JE , (2013) PROPOSED VERTICAL EXPANSION TUNNEL.AIAA JOURNAL. VOL. 51. ISSUE 12. P. 2792-2799 | 9 | 45% | 1 |
7 | BISHOP, AI , MCINTYRE, TJ , LITTLETON, BN , RUBINSZTEIN-DUNLOP, H , (2004) OH CONCENTRATION AND TEMPERATURE MEASUREMENTS BY USE OF NEAR-RESONANT HOLOGRAPHIC INTERFEROMETRY.APPLIED OPTICS. VOL. 43. ISSUE 35. P. 6384 -6390 | 6 | 86% | 1 |
8 | EICHMANN, TN , MCINTYRE, TJ , BISHOP, AI , VAKATA, S , RUBINSZTEIN-DUNLOP, H , (2007) THREE-DIMENSIONAL EFFECTS ON LINE-OF-SIGHT VISUALIZATION MEASUREMENTS OF SUPERSONIC AND HYPERSONIC FLOW OVER CYLINDERS.SHOCK WAVES. VOL. 16. ISSUE 4-5. P. 299-307 | 7 | 54% | 0 |
9 | GILDFIND, DE , JACOBS, PA , MORGAN, RG , (2013) VIBRATION ISOLATION IN A FREE-PISTON DRIVEN EXPANSION TUBE FACILITY.SHOCK WAVES. VOL. 23. ISSUE 5. P. 431-438 | 3 | 100% | 1 |
10 | DATEY, A , THAHA, CSA , PATIL, SR , GOPALAN, J , CHAKRAVORTTY, D , (2016) ENHANCING THE EFFICIENCY OF DESENSITIZING AGENTS WITH SHOCKWAVE TREATMENT - A NEW PARADIGM IN DENTINAL HYPERSENSITIVITY MANAGEMENT.RSC ADVANCES. VOL. 6. ISSUE 73. P. 68973 -68978 | 6 | 46% | 0 |
Classes with closest relation at Level 1 |