Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
35127 | 102 | 18.9 | 25% |
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 |
3258 | 2 | VORTEX TUBE//VORTEX METHOD//RANQUE HILSCH VORTEX TUBE | 1965 |
35127 | 1 | HARTMANN WHISTLE//DIFFERENTIAL TURBULENCE MODELS//HARTMANN RESONANCE TUBE | 102 |
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 | HARTMANN WHISTLE | authKW | 935524 | 5% | 63% | 5 |
2 | DIFFERENTIAL TURBULENCE MODELS | authKW | 598738 | 2% | 100% | 2 |
3 | HARTMANN RESONANCE TUBE | authKW | 598738 | 2% | 100% | 2 |
4 | HARTMANN SPRENGER TUBE | authKW | 598738 | 2% | 100% | 2 |
5 | NARROW CHANNEL APPROXIMATION | authKW | 598738 | 2% | 100% | 2 |
6 | TEMPERATURE RECOVERY COEFFICIENT | authKW | 598738 | 2% | 100% | 2 |
7 | UNDERWATER COMBUSTION | authKW | 538862 | 3% | 60% | 3 |
8 | GAS SUCTION | authKW | 399157 | 2% | 67% | 2 |
9 | ACOUSTIC RESONANCE HEATING | authKW | 299369 | 1% | 100% | 1 |
10 | ADV AEROSP TECHNOLKWANAK GU | address | 299369 | 1% | 100% | 1 |
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 | 1684 | 20% | 0% | 20 |
2 | Mechanics | 1659 | 44% | 0% | 45 |
3 | Engineering, Mechanical | 777 | 28% | 0% | 29 |
4 | Physics, Fluids & Plasmas | 512 | 18% | 0% | 18 |
5 | Thermodynamics | 362 | 16% | 0% | 16 |
6 | Acoustics | 317 | 11% | 0% | 11 |
7 | Physics, Applied | 24 | 13% | 0% | 13 |
8 | Engineering, General | 21 | 4% | 0% | 4 |
9 | Mathematics, Interdisciplinary Applications | 4 | 2% | 0% | 2 |
10 | Energy & Fuels | 4 | 3% | 0% | 3 |
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 | ADV AEROSP TECHNOLKWANAK GU | 299369 | 1% | 100% | 1 |
2 | KAZAN AVIAT | 42765 | 1% | 14% | 1 |
3 | MULTIPHASE FLOWS | 21382 | 1% | 7% | 1 |
4 | ENGN UNIV | 14967 | 1% | 5% | 1 |
5 | PROP | 9351 | 2% | 2% | 2 |
6 | GAS DYNAM TURBULENCE | 8551 | 1% | 3% | 1 |
7 | ISOGO NUCL ENGN | 8089 | 1% | 3% | 1 |
8 | COMBUST DEV | 7876 | 1% | 3% | 1 |
9 | SIR HARRY RICARDO S | 7482 | 1% | 3% | 1 |
10 | SS KUTATELADZE THERMOPHYS | 6368 | 1% | 2% | 1 |
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 | FLUID DYNAMICS | 53771 | 15% | 1% | 15 |
2 | IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 22586 | 4% | 2% | 4 |
3 | JOURNAL OF MECHANICAL ENGINEERING SCIENCE | 13920 | 2% | 2% | 2 |
4 | HIGH TEMPERATURE | 13149 | 13% | 0% | 13 |
5 | SCIENCE AND TECHNOLOGY OF ENERGETIC MATERIALS | 1329 | 1% | 0% | 1 |
6 | AIAA JOURNAL | 1267 | 7% | 0% | 7 |
7 | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | 1251 | 1% | 0% | 1 |
8 | FLOW TURBULENCE AND COMBUSTION | 1202 | 2% | 0% | 2 |
9 | INTERNATIONAL JOURNAL OF AEROACOUSTICS | 1158 | 1% | 0% | 1 |
10 | CENTRAL EUROPEAN JOURNAL OF ENERGETIC MATERIALS | 1087 | 1% | 0% | 1 |
Author Key Words |
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 | NARAYANAN, S , SRINIVASAN, K , SUNDARARAJAN, T , (2013) ACOUSTIC CHARACTERISTICS OF EXTERNAL CHAMFERED HARTMANN WHISTLES.APPLIED ACOUSTICS. VOL. 74. ISSUE 9. P. 1104-1116 | 11 | 100% | 1 |
2 | RAMAN, G , SRINIVASAN, K , (2009) THE POWERED RESONANCE TUBE: FROM HARTMANN'S DISCOVERY TO CURRENT ACTIVE FLOW CONTROL APPLICATIONS.PROGRESS IN AEROSPACE SCIENCES. VOL. 45. ISSUE 4-5. P. 97 -123 | 23 | 50% | 12 |
3 | NARAYANAN, S , SRINIVASAN, K , SUNDARARAJAN, T , (2014) EFFECT OF LIP THICKNESS ON THE AERO-ACOUSTIC FEATURES OF HARTMANN WHISTLE.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. VOL. 228. ISSUE 8. P. 1302-1313 | 9 | 100% | 0 |
4 | NARAYANAN, S , SRINIVASAN, K , SUNDARARAJAN, T , RAMAMURTHI, K , (2011) ACOUSTIC CHARACTERISTICS OF CHAMFERED HARTMANN WHISTLES.JOURNAL OF SOUND AND VIBRATION. VOL. 330. ISSUE 11. P. 2470-2496 | 9 | 90% | 2 |
5 | NARAYANAN, S , SRINIVASAN, K , SUNDARARAJAN, T , (2014) AERO-ACOUSTIC FEATURES OF INTERNAL AND EXTERNAL CHAMFERED HARTMANN WHISTLES: A COMPARATIVE STUDY.JOURNAL OF SOUND AND VIBRATION. VOL. 333. ISSUE 3. P. 774-787 | 8 | 89% | 1 |
6 | VINOTH, BR , THROVAGUNTA, P , RATHAKRISHNAN, E , (2012) EFFECT OF TUBE LIP THICKNESS ON THE PERFORMANCE OF HARTMANN-SPRENGER TUBES.PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. VOL. 226. ISSUE G1. P. 74-87 | 8 | 89% | 2 |
7 | LEONT'EV, AI , LUSHCHIK, VG , MAKAROVA, MS , (2012) TEMPERATURE STRATIFICATION UNDER SUCTION OF THE BOUNDARY LAYER FROM A SUPERSONIC FLOW.HIGH TEMPERATURE. VOL. 50. ISSUE 6. P. 739-743 | 7 | 100% | 3 |
8 | MICHAEL, E , NARAYANAN, S , JALEEL, HA , (2015) NUMERICAL SIMULATION OF JET FLOW IMPINGING ON A SHIELDED HARTMANN WHISTLE.INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES. VOL. 16. ISSUE 2. P. 123 -136 | 7 | 88% | 1 |
9 | BURTSEV, SA , LEONTIEV, AI , (2014) STUDY OF THE INFLUENCE OF DISSIPATIVE EFFECTS ON THE TEMPERATURE STRATIFICATION IN GAS FLOWS (REVIEW).HIGH TEMPERATURE. VOL. 52. ISSUE 2. P. 297 -307 | 14 | 41% | 2 |
10 | MAKAROV, MS , MAKAROVA, SN , (2013) EFFICIENCY OF ENERGY SEPARATION AT COMPRESSIBLE GAS FLOW IN A PLANAR DUCT.THERMOPHYSICS AND AEROMECHANICS. VOL. 20. ISSUE 6. P. 757-767 | 7 | 78% | 1 |
Classes with closest relation at Level 1 |