Class information for: |
Basic class information |
Class id | #P | Avg. number of references |
Database coverage of references |
---|---|---|---|
28339 | 209 | 20.3 | 29% |
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 |
124 | 2 | JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME//MECHANICS//ENGINEERING, MECHANICAL | 24158 |
28339 | 1 | TRANSPIRATION COOLING//COMPRESSIBLE OR INCOMPRESSIBLE FLUID//NON ISOTHERMAL BLOWING | 209 |
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 | TRANSPIRATION COOLING | authKW | 1431236 | 11% | 43% | 23 |
2 | COMPRESSIBLE OR INCOMPRESSIBLE FLUID | authKW | 292205 | 1% | 100% | 2 |
3 | NON ISOTHERMAL BLOWING | authKW | 292205 | 1% | 100% | 2 |
4 | STRATEG DEF COMMAND | address | 292205 | 1% | 100% | 2 |
5 | SUPERSONIC EXPERIMENT | authKW | 292205 | 1% | 100% | 2 |
6 | NOSE CONE | authKW | 259733 | 2% | 44% | 4 |
7 | THERM LYON | address | 208283 | 6% | 12% | 12 |
8 | TANGENTIAL BLOWING | authKW | 194802 | 1% | 67% | 2 |
9 | UMR 5008 THERM LYON | address | 194802 | 1% | 67% | 2 |
10 | AERODYNAMIC COMPENSATION | authKW | 146102 | 0% | 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 | 7961 | 30% | 0% | 62 |
2 | Thermodynamics | 5249 | 41% | 0% | 85 |
3 | Engineering, Mechanical | 3740 | 43% | 0% | 90 |
4 | Mechanics | 1927 | 33% | 0% | 70 |
5 | Physics, Fluids & Plasmas | 96 | 6% | 0% | 12 |
6 | Energy & Fuels | 31 | 5% | 0% | 10 |
7 | Mathematics, Interdisciplinary Applications | 15 | 2% | 0% | 5 |
8 | Engineering, Marine | 13 | 0% | 0% | 1 |
9 | Engineering, General | 12 | 2% | 0% | 5 |
10 | Materials Science, Composites | 6 | 1% | 0% | 2 |
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 | STRATEG DEF COMMAND | 292205 | 1% | 100% | 2 |
2 | THERM LYON | 208283 | 6% | 12% | 12 |
3 | UMR 5008 THERM LYON | 194802 | 1% | 67% | 2 |
4 | BAUWEISEN STRUKTURTECHNOL | 146102 | 0% | 100% | 1 |
5 | INT METODOS NUMERICOS INGN CIMNE | 146102 | 0% | 100% | 1 |
6 | MECH ENGN THERMOSCI | 146102 | 0% | 100% | 1 |
7 | MINIST EDUC CHINABEIJING UTILIZAT REDU | 146102 | 0% | 100% | 1 |
8 | PERFORMANCE FLYING QUAL FLIGHT | 146102 | 0% | 100% | 1 |
9 | STOSS WELLEN | 146102 | 0% | 100% | 1 |
10 | TESTING TECH FLIGHT | 146102 | 0% | 100% | 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 | JOURNAL OF SPACECRAFT AND ROCKETS | 13786 | 10% | 0% | 20 |
2 | JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER | 8305 | 6% | 0% | 12 |
3 | AIAA JOURNAL | 5586 | 10% | 0% | 21 |
4 | INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER | 3392 | 10% | 0% | 20 |
5 | REVUE GENERALE DE THERMIQUE | 3052 | 1% | 1% | 3 |
6 | JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME | 2819 | 4% | 0% | 9 |
7 | HIGH TEMPERATURE | 2419 | 4% | 0% | 8 |
8 | INTERNATIONAL JOURNAL OF ENGINEERING FLUID MECHANICS | 2115 | 0% | 1% | 1 |
9 | AEROSPACE AMERICA | 1822 | 1% | 1% | 2 |
10 | JOURNAL OF PROPULSION AND POWER | 1612 | 3% | 0% | 7 |
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 | KELLER, MA , KLOKER, MJ , OLIVIER, H , (2015) INFLUENCE OF COOLING-GAS PROPERTIES ON FILM-COOLING EFFECTIVENESS IN SUPERSONIC FLOW.JOURNAL OF SPACECRAFT AND ROCKETS. VOL. 52. ISSUE 5. P. 1443 -1455 | 12 | 86% | 0 |
2 | SHEN, L , WANG, JH , DONG, WJ , PU, J , PENG, JL , QU, DJ , CHEN, LZ , (2016) AN EXPERIMENTAL INVESTIGATION ON TRANSPIRATION COOLING WITH PHASE CHANGE UNDER SUPERSONIC CONDITION.APPLIED THERMAL ENGINEERING. VOL. 105. ISSUE . P. 549 -556 | 12 | 71% | 0 |
3 | XU, GQ , LIU, YP , LUO, X , MA, JD , LI, HW , (2015) EXPERIMENTAL INVESTIGATION OF TRANSPIRATION COOLING FOR SINTERED WOVEN WIRE MESH STRUCTURES.INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER. VOL. 91. ISSUE . P. 898 -907 | 11 | 73% | 0 |
4 | KELLER, MA , KLOKER, MJ , (2017) DIRECT NUMERICAL SIMULATION OF FOREIGN-GAS FILM COOLING IN SUPERSONIC BOUNDARY-LAYER FLOW.AIAA JOURNAL. VOL. 55. ISSUE 1. P. 99 -111 | 14 | 50% | 0 |
5 | MA, JD , LUO, X , LI, HW , LIU, YP , (2016) AN EXPERIMENTAL INVESTIGATION ON TRANSPIRATION COOLING BASED ON THE MULTILAMINATED SINTERED WOVEN WIRE MESH STRUCTURES.JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS. VOL. 8. ISSUE 3. P. - | 13 | 54% | 0 |
6 | PENG, W , JIANG, PX , (2014) EFFECT OF SHOCK WAVES ON SUPERSONIC FILM COOLING WITH A SLOTTED WALL.APPLIED THERMAL ENGINEERING. VOL. 62. ISSUE 1. P. 187 -196 | 8 | 73% | 5 |
7 | DAHMEN, W , MULLER, S , ROM, M , SCHWEIKERT, S , SELZER, M , VON WOLFERSDORF, J , (2015) NUMERICAL BOUNDARY LAYER INVESTIGATIONS OF TRANSPIRATION-COOLED TURBULENT CHANNEL FLOW.INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER. VOL. 86. ISSUE . P. 90 -100 | 10 | 56% | 1 |
8 | WANG, JH , ZHAO, LJ , WANG, XC , MA, J , LIN, J , (2014) AN EXPERIMENTAL INVESTIGATION ON TRANSPIRATION COOLING OF WEDGE SHAPED NOSE CONE WITH LIQUID COOLANT.INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER. VOL. 75. ISSUE . P. 442-449 | 7 | 78% | 4 |
9 | ZHAO, LJ , WANG, JH , MA, J , LIN, J , PENG, JL , QU, DJ , CHEN, LZ , (2014) AN EXPERIMENTAL INVESTIGATION ON TRANSPIRATION COOLING UNDER SUPERSONIC CONDITION USING A NOSE CONE MODEL.INTERNATIONAL JOURNAL OF THERMAL SCIENCES. VOL. 84. ISSUE . P. 207 -213 | 8 | 67% | 2 |
10 | HUANG, Z , XIONG, YB , LIU, YQ , JIANG, PX , ZHU, YH , (2015) EXPERIMENTAL INVESTIGATION OF FULL-COVERAGE EFFUSION COOLING THROUGH PERFORATED FLAT PLATES.APPLIED THERMAL ENGINEERING. VOL. 76. ISSUE . P. 76 -85 | 6 | 75% | 2 |
Classes with closest relation at Level 1 |