Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
29416 | 186 | 14.6 | 21% |
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 |
29416 | 1 | PRANDTL MEYER FUNCTION//SETTLING CHAMBER//CALORICALLY IMPERFECT GAS | 186 |
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 | PRANDTL MEYER FUNCTION | authKW | 820846 | 3% | 100% | 5 |
2 | SETTLING CHAMBER | authKW | 618785 | 4% | 54% | 7 |
3 | CALORICALLY IMPERFECT GAS | authKW | 492507 | 2% | 100% | 3 |
4 | TEST GAS | authKW | 369379 | 2% | 75% | 3 |
5 | AXISYMMETRIC MINIMUM LENGTH NOZZLE | authKW | 328338 | 1% | 100% | 2 |
6 | COMPLEXES OF AERODYNAMIC DERIVATIVES | authKW | 328338 | 1% | 100% | 2 |
7 | GASDYNAMIC DESIGN | authKW | 328338 | 1% | 100% | 2 |
8 | HIGH ENTHALPY FACILITY | authKW | 328338 | 1% | 100% | 2 |
9 | HIGH ENTHALPY HOTSHOT WIND TUNNEL | authKW | 328338 | 1% | 100% | 2 |
10 | HIGH ENTHALPY SHORT DURATION WIND TUNNEL | authKW | 328338 | 1% | 100% | 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 | 4909 | 25% | 0% | 46 |
2 | Thermodynamics | 3540 | 35% | 0% | 66 |
3 | Engineering, General | 2024 | 25% | 0% | 47 |
4 | Energy & Fuels | 981 | 24% | 0% | 44 |
5 | Mechanics | 871 | 24% | 0% | 45 |
6 | Engineering, Chemical | 535 | 23% | 0% | 43 |
7 | Materials Science, Multidisciplinary | 212 | 26% | 0% | 48 |
8 | Engineering, Mechanical | 94 | 8% | 0% | 15 |
9 | Instruments & Instrumentation | 73 | 7% | 0% | 13 |
10 | Physics, Applied | 57 | 14% | 0% | 26 |
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 | KHRISTIANOVICH THEORET PL MECH | 196140 | 13% | 5% | 24 |
2 | HYDROAEROMECH | 164169 | 1% | 100% | 1 |
3 | AERONAUT SPACE STUDIES | 131333 | 1% | 40% | 2 |
4 | SCI ENGINEER | 46902 | 1% | 14% | 2 |
5 | GASL | 41041 | 1% | 25% | 1 |
6 | STATE OPTIMAS | 16415 | 1% | 10% | 1 |
7 | GEOL OIL GAS | 13679 | 1% | 8% | 1 |
8 | AUTOMATIZAT | 13677 | 1% | 4% | 2 |
9 | THEORET PL MECH | 9536 | 5% | 1% | 10 |
10 | HIGH SPEED AERODYNAM | 9119 | 1% | 6% | 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 | THERMOPHYSICS AND AEROMECHANICS | 132315 | 11% | 4% | 21 |
2 | COMBUSTION EXPLOSION AND SHOCK WAVES | 79904 | 21% | 1% | 39 |
3 | JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS | 19863 | 6% | 1% | 11 |
4 | JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME | 5905 | 5% | 0% | 9 |
5 | SHOCK WAVES | 5548 | 3% | 1% | 6 |
6 | PROGRESS IN AEROSPACE SCIENCES | 3546 | 2% | 1% | 3 |
7 | AIAA JOURNAL | 3196 | 8% | 0% | 15 |
8 | IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 3094 | 1% | 1% | 2 |
9 | CHINESE JOURNAL OF AERONAUTICS | 2100 | 2% | 0% | 4 |
10 | INVERSE PROBLEMS IN ENGINEERING | 1146 | 1% | 1% | 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 | ZABAYKIN, VA , SMOGELEV, AA , (2007) HYDROGEN COMBUSTION IN AN AXISYMMETRIC DUCT WITH A SUPERSONIC AIR FLOW.COMBUSTION EXPLOSION AND SHOCK WAVES. VOL. 43. ISSUE 3. P. 247-252 | 7 | 100% | 0 |
2 | ZHANG, GH , BRAVERMAN, B , KAWASAKI, A , VULETIC, V , (2015) NOTE: FAST COMPACT LASER SHUTTER USING A DIRECT CURRENT MOTOR AND THREE-DIMENSIONAL PRINTING.REVIEW OF SCIENTIFIC INSTRUMENTS. VOL. 86. ISSUE 12. P. - | 5 | 100% | 0 |
3 | ABADA, O , ZEBBICHE, T , EL-HIRTSI, AA , (2014) THREE-DIMENSIONAL SUPERSONIC MINIMUM LENGTH NOZZLE DESIGN AT HIGH TEMPERATURE FOR ARBITRARY EXIT CROSS SECTION.ARABIAN JOURNAL FOR SCIENCE AND ENGINEERING. VOL. 39. ISSUE 11. P. 8233 -8245 | 5 | 100% | 0 |
4 | USKOV, VN , MOSTOVYKH, PS , (2016) THE FLOW GRADIENTS IN THE VICINITY OF A SHOCK WAVE FOR A THERMODYNAMICALLY IMPERFECT GAS.SHOCK WAVES. VOL. 26. ISSUE 6. P. 693 -708 | 5 | 83% | 0 |
5 | LATYPOV, AF , (2015) FUNCTIONAL MATHEMATICAL MODEL OF A HYDROGEN-DRIVEN COMBUSTION CHAMBER FOR A SCRAMJET.JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS. VOL. 56. ISSUE 5. P. 799 -812 | 4 | 100% | 0 |
6 | BAUER, M , FRANZREB, PP , SPETHMANN, N , WIDERA, A , (2014) NOTE: RELIABLE LOW-VIBRATION PIEZO-MECHANICAL SHUTTER.REVIEW OF SCIENTIFIC INSTRUMENTS. VOL. 85. ISSUE 9. P. - | 4 | 100% | 0 |
7 | LATYPOV, AF , (2013) EXERGY METHOD FOR ESTIMATING THE RAMJET SPECIFIC IMPULSE.THERMOPHYSICS AND AEROMECHANICS. VOL. 20. ISSUE 5. P. 539-552 | 4 | 100% | 0 |
8 | MARTINEZ, S , HERNANDEZ, L , REYES, D , GOMEZ, E , IVORY, M , DAVISON, C , AUBIN, S , (2011) FAST, SMALL, AND LOW VIBRATION MECHANICAL LASER SHUTTERS.REVIEW OF SCIENTIFIC INSTRUMENTS. VOL. 82. ISSUE 4. P. - | 4 | 100% | 5 |
9 | ZEBBICHE, T , (2011) STAGNATION TEMPERATURE EFFECT ON THE SUPERSONIC AXISYMMETRIC MINIMUM LENGTH NOZZLE DESIGN WITH APPLICATION FOR AIR.ADVANCES IN SPACE RESEARCH. VOL. 48. ISSUE 10. P. 1656-1675 | 4 | 100% | 3 |
10 | VORONTSOV, SS , ZABAIKIN, VA , SMOGOLEV, AA , TRET'YAKOV, PK , (2003) VORTEX STRUCTURES IN COMBUSTION OF HYDROGEN IN A SUPERSONIC COCURRENT AIR STREAM.COMBUSTION EXPLOSION AND SHOCK WAVES. VOL. 39. ISSUE 2. P. 119-123 | 5 | 100% | 0 |
Classes with closest relation at Level 1 |