Class information for: |
Basic class information |
ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
---|---|---|---|
7593 | 1270 | 21.9 | 26% |
Classes in level above (level 2) |
ID, lev. above |
Publications | Label for level above |
---|---|---|
693 | 12356 | PROPELLANTS EXPLOSIVES PYROTECHNICS//ENERGETIC MATERIALS//JOURNAL OF ENERGETIC MATERIALS |
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 | REGRESSION RATE | Author keyword | 33 | 83% | 1% | 19 |
2 | HYBRID ROCKET MOTOR | Author keyword | 30 | 79% | 1% | 19 |
3 | EROSIVE BURNING | Author keyword | 21 | 85% | 1% | 11 |
4 | HYBRID ROCKET | Author keyword | 15 | 59% | 1% | 17 |
5 | HYBRID ROCKET COMBUSTION | Author keyword | 9 | 83% | 0% | 5 |
6 | SIMULAT ADV ROCKETS | Address | 9 | 26% | 2% | 29 |
7 | SOLID PROPELLANT COMBUSTION | Author keyword | 8 | 70% | 1% | 7 |
8 | FUEL REGRESSION RATE | Author keyword | 8 | 75% | 0% | 6 |
9 | SOLID PROPELLANTS | Author keyword | 6 | 28% | 1% | 17 |
10 | HYBRID ROCKET PROPULSION | Author keyword | 4 | 75% | 0% | 3 |
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 | REGRESSION RATE | 33 | 83% | 1% | 19 | Search REGRESSION+RATE | Search REGRESSION+RATE |
2 | HYBRID ROCKET MOTOR | 30 | 79% | 1% | 19 | Search HYBRID+ROCKET+MOTOR | Search HYBRID+ROCKET+MOTOR |
3 | EROSIVE BURNING | 21 | 85% | 1% | 11 | Search EROSIVE+BURNING | Search EROSIVE+BURNING |
4 | HYBRID ROCKET | 15 | 59% | 1% | 17 | Search HYBRID+ROCKET | Search HYBRID+ROCKET |
5 | HYBRID ROCKET COMBUSTION | 9 | 83% | 0% | 5 | Search HYBRID+ROCKET+COMBUSTION | Search HYBRID+ROCKET+COMBUSTION |
6 | SOLID PROPELLANT COMBUSTION | 8 | 70% | 1% | 7 | Search SOLID+PROPELLANT+COMBUSTION | Search SOLID+PROPELLANT+COMBUSTION |
7 | FUEL REGRESSION RATE | 8 | 75% | 0% | 6 | Search FUEL+REGRESSION+RATE | Search FUEL+REGRESSION+RATE |
8 | SOLID PROPELLANTS | 6 | 28% | 1% | 17 | Search SOLID+PROPELLANTS | Search SOLID+PROPELLANTS |
9 | HYBRID ROCKET PROPULSION | 4 | 75% | 0% | 3 | Search HYBRID+ROCKET+PROPULSION | Search HYBRID+ROCKET+PROPULSION |
10 | LIQUID OXIDIZER | 4 | 75% | 0% | 3 | Search LIQUID+OXIDIZER | Search LIQUID+OXIDIZER |
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 | SOLID PROPELLANT ROCKET | 77 | 96% | 2% | 24 |
2 | SURFACE MASS INJECTION | 32 | 85% | 1% | 17 |
3 | POROUS CHAMBER | 27 | 92% | 1% | 11 |
4 | SOLID ROCKET MOTORS | 27 | 62% | 2% | 28 |
5 | REGRESSION RATE | 18 | 83% | 1% | 10 |
6 | REGRESSING WALLS | 17 | 100% | 1% | 8 |
7 | REGRESSION RATE BEHAVIOR | 17 | 100% | 1% | 8 |
8 | UNSTEADY FLOW EVOLUTION | 15 | 73% | 1% | 11 |
9 | ROCKET MOTOR | 13 | 67% | 1% | 12 |
10 | PROPELLANT ROCKET | 13 | 80% | 1% | 8 |
Journals |
Reviews |
Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
---|---|---|---|---|
Modeling of combustion and ignition of solid-propellant ingredients | 2007 | 23 | 70 | 66% |
Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines | 2012 | 4 | 14 | 86% |
Analysis of unsteady solid-propellant combustion models (Review) | 2008 | 5 | 31 | 97% |
Laminate propellant combustion (Review) - 2. Theoretical investigations | 2006 | 6 | 14 | 100% |
Hybrid Rocket Technology | 2011 | 1 | 12 | 100% |
Combustion of energetic materials in an acoustic field (review) | 2005 | 6 | 8 | 88% |
On the Lagrangian optimization of wall-injected flows: from the Hart-McClure potential to the Taylor-Culick rotational motion | 2010 | 1 | 24 | 92% |
Critical review of phenomenological models for studying transient combustion of solid propellants | 2010 | 1 | 10 | 90% |
Solid fuel ramjet combustor design | 1998 | 15 | 26 | 73% |
Laminate propellant combustion (review) - 1. Experimental investigations | 2005 | 2 | 7 | 100% |
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 | SIMULAT ADV ROCKETS | 9 | 26% | 2.3% | 29 |
2 | AERODYNAM ENERGET MODELING | 3 | 33% | 0.6% | 7 |
3 | FUNDAMENTAL PL ENERGET | 2 | 32% | 0.5% | 6 |
4 | FLUID MECH INTERNAL BALLIST | 2 | 67% | 0.2% | 2 |
5 | ROCKET PROP DIRECTORATE | 2 | 67% | 0.2% | 2 |
6 | PROP SCI BRANCH | 2 | 50% | 0.2% | 3 |
7 | COMBUST RD SECT | 1 | 100% | 0.2% | 2 |
8 | FINE ROCKET PROP | 1 | 50% | 0.2% | 2 |
9 | PROP GRP | 1 | 50% | 0.2% | 2 |
10 | ROCKETS MISSILES | 1 | 100% | 0.2% | 2 |
Related classes at same level (level 1) |
Rank | Relatedness score | Related classes |
---|---|---|
1 | 0.0000158889 | AMMONIUM PERCHLORATE//EXPLOSION DELAY//AMMONIUM PERCHLORATE AP |
2 | 0.0000140503 | DEV TEST//GRAIN DESIGN//SATELLITE LAUNCH VEHICLE |
3 | 0.0000127098 | CNPM//RADIANT FLUX DENSITY//COMPOSITE POLYMERIC MATERIAL |
4 | 0.0000098525 | GLYCIDYL AZIDE POLYMER GAP//ENERGETIC PLASTICIZER//PROPELLANT BINDER |
5 | 0.0000098091 | AMMONIUM DINITRAMIDE//DINITRAMIDE//DINITRAMIDE SALTS |
6 | 0.0000085295 | THERMITES//THERMITE//METAL COMBUSTION |
7 | 0.0000064982 | SIDE DUMP COMBUSTOR//COMBUSTOR FLOW//JET IMPINGEMENTS |
8 | 0.0000053869 | CL 20//PROPELLANTS EXPLOSIVES PYROTECHNICS//HNIW |
9 | 0.0000050065 | RESTRICTED SHOCK SEPARATION//FREE SHOCK SEPARATION//SIDE LOADS |
10 | 0.0000047922 | LOCAL DEFECT CORRECTION//ENGN KITA KU//FAST ADAPTIVE COMPOSITE GRID METHOD |