Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 5690 | 1521 | 22.6 | 34% |
Classes in level above (level 2) |
| ID, lev. above |
Publications | Label for level above |
|---|---|---|
| 1797 | 5767 | JOURNAL OF SPACECRAFT AND ROCKETS//HYPERSON//SCRAMJET |
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 | SCRAMJET | Author keyword | 89 | 58% | 7% | 102 |
| 2 | SUPERSONIC COMBUSTION | Author keyword | 57 | 55% | 5% | 71 |
| 3 | JOURNAL OF PROPULSION AND POWER | Journal | 55 | 11% | 31% | 464 |
| 4 | CAVITY FLAMEHOLDER | Author keyword | 34 | 93% | 1% | 13 |
| 5 | SCI TECHNOL SCRAMJET | Address | 32 | 38% | 4% | 66 |
| 6 | SCRAMJET COMBUSTOR | Author keyword | 23 | 79% | 1% | 15 |
| 7 | HYPERSON | Address | 22 | 42% | 3% | 41 |
| 8 | COMBINED PROPULS GRP | Address | 20 | 100% | 1% | 9 |
| 9 | AEROSPACE PROPULSION SYSTEM | Author keyword | 18 | 56% | 1% | 22 |
| 10 | SHOCK TRAIN | Author keyword | 17 | 72% | 1% | 13 |
Web of Science journal categories |
Author Key Words |
| 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 |
LCSH search | Wikipedia search |
|---|---|---|---|---|---|---|---|
| 1 | SCRAMJET | 89 | 58% | 7% | 102 | Search SCRAMJET | Search SCRAMJET |
| 2 | SUPERSONIC COMBUSTION | 57 | 55% | 5% | 71 | Search SUPERSONIC+COMBUSTION | Search SUPERSONIC+COMBUSTION |
| 3 | CAVITY FLAMEHOLDER | 34 | 93% | 1% | 13 | Search CAVITY+FLAMEHOLDER | Search CAVITY+FLAMEHOLDER |
| 4 | SCRAMJET COMBUSTOR | 23 | 79% | 1% | 15 | Search SCRAMJET+COMBUSTOR | Search SCRAMJET+COMBUSTOR |
| 5 | AEROSPACE PROPULSION SYSTEM | 18 | 56% | 1% | 22 | Search AEROSPACE+PROPULSION+SYSTEM | Search AEROSPACE+PROPULSION+SYSTEM |
| 6 | SHOCK TRAIN | 17 | 72% | 1% | 13 | Search SHOCK+TRAIN | Search SHOCK+TRAIN |
| 7 | WAVERIDER | 15 | 63% | 1% | 15 | Search WAVERIDER | Search WAVERIDER |
| 8 | SCRAMJET ENGINE | 14 | 60% | 1% | 15 | Search SCRAMJET+ENGINE | Search SCRAMJET+ENGINE |
| 9 | HYPERSONIC INLET | 14 | 65% | 1% | 13 | Search HYPERSONIC+INLET | Search HYPERSONIC+INLET |
| 10 | AEROSPACE PROPULSION SYSTEMS | 14 | 100% | 0% | 7 | Search AEROSPACE+PROPULSION+SYSTEMS | Search AEROSPACE+PROPULSION+SYSTEMS |
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 | UNSTART | 73 | 96% | 2% | 23 |
| 2 | TRANSVERSE INJECTION | 55 | 92% | 1% | 22 |
| 3 | HYPERSONIC INLET | 49 | 94% | 1% | 17 |
| 4 | ELLIPTIC SHAPE TRANSITION | 42 | 94% | 1% | 15 |
| 5 | SCRAMJET ENGINE | 35 | 89% | 1% | 16 |
| 6 | SUPERSONIC COMBUSTION | 32 | 62% | 2% | 33 |
| 7 | SCRAMJET COMBUSTOR | 31 | 66% | 2% | 29 |
| 8 | START UNSTART | 26 | 100% | 1% | 11 |
| 9 | SCRAMJET | 26 | 63% | 2% | 26 |
| 10 | FLAMEHOLDER | 21 | 75% | 1% | 15 |
Journals |
| 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 | JOURNAL OF PROPULSION AND POWER | 55 | 11% | 31% | 464 |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Scramjet engines: The first forty years | 2001 | 104 | 9 | 89% |
| Shock train and pseudo-shock phenomena in internal gas flows | 1999 | 90 | 45 | 64% |
| Fluid phenomena in scramjet combustion systems | 1996 | 59 | 10 | 50% |
| Progress in research on mixing techniques for transverse injection flow fields in supersonic crossflows | 2013 | 3 | 47 | 77% |
| Scramjets and shock tunnels - The Queensland experience | 2005 | 18 | 31 | 77% |
| Effects of wall cooling on performance parameters of hypersonic inlets | 2009 | 7 | 8 | 88% |
| A review of fuel pre-injection in supersonic, chemically reacting flows | 2007 | 6 | 17 | 88% |
| Supersonic jet and crossflow interaction: Computational modeling | 2013 | 7 | 49 | 29% |
| Operation pattern classification of hypersonic inlets | 2009 | 4 | 11 | 73% |
| A review of numerical simulation and modeling of combustion in scramjets | 2015 | 0 | 11 | 91% |
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 | SCI TECHNOL SCRAMJET | 32 | 38% | 4.3% | 66 |
| 2 | HYPERSON | 22 | 42% | 2.7% | 41 |
| 3 | COMBINED PROPULS GRP | 20 | 100% | 0.6% | 9 |
| 4 | COMBINED PROP GRP | 15 | 88% | 0.5% | 7 |
| 5 | HYPERSON PROP | 11 | 100% | 0.4% | 6 |
| 6 | RAMJET PROP | 11 | 100% | 0.4% | 6 |
| 7 | WIND TUNNEL | 10 | 58% | 0.7% | 11 |
| 8 | RAMJET PROPULS | 8 | 100% | 0.3% | 5 |
| 9 | KAKUDA SPACE | 7 | 44% | 0.8% | 12 |
| 10 | HYPERSON AIRBREATHING PROPULS BRANCH | 6 | 80% | 0.3% | 4 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000193639 | OPPOSING JET//HYPERSONIC SHOCK TUNNEL//FORWARD FACING CAVITY |
| 2 | 0.0000185209 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
| 3 | 0.0000122306 | SETTLING CHAMBER//SCI SYST ANAL//CHLORINE TRIFLUORIDE OXIDE |
| 4 | 0.0000095222 | SIDE DUMP COMBUSTOR//COMBUSTOR FLOW//JET IMPINGEMENTS |
| 5 | 0.0000094687 | SPACE ENGN PROGRAM//CARRIER VEHICLES//MASS DRIVER |
| 6 | 0.0000085019 | RESTRICTED SHOCK SEPARATION//FREE SHOCK SEPARATION//SIDE LOADS |
| 7 | 0.0000081136 | TRAPPED VORTEX COMBUSTOR//TRAPPED VORTEX//SCI TECHNOL AEROENGINES AEROTHERMO |
| 8 | 0.0000080909 | FLEXIBLE AIR BREATHING HYPERSONIC VEHICLE//FLEXIBLE AIR BREATHING HYPERSONIC VEHICLE FAHV//AIRBREATHING HYPERSONIC VEHICLE |
| 9 | 0.0000078424 | JETS IN CROSSFLOW//JET IN CROSS FLOW//JET IN CROSSFLOW |
| 10 | 0.0000068060 | CARBUNCLE PHENOMENON//SHOCK INSTABILITY//MACH UNIFORM |