Class information for: |
Basic class information |
| ID | Publications | Average number of references |
Avg. shr. active ref. in WoS |
|---|---|---|---|
| 20068 | 414 | 20.0 | 25% |
Classes in level above (level 2) |
| ID, lev. above |
Publications | Label for level above |
|---|---|---|
| 429 | 15725 | JOURNAL OF COMPUTATIONAL PHYSICS//INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS//COMPUTERS & FLUIDS |
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 | RESTRICTED SHOCK SEPARATION | Author keyword | 38 | 93% | 3% | 14 |
| 2 | FREE SHOCK SEPARATION | Author keyword | 15 | 82% | 2% | 9 |
| 3 | SIDE LOADS | Author keyword | 13 | 67% | 3% | 12 |
| 4 | PROP STRUCT THERMAL FLUIDS ANAL | Address | 8 | 100% | 1% | 5 |
| 5 | LIQUID ENGINE MAIN PROP SYST BRANCH | Address | 6 | 100% | 1% | 4 |
| 6 | NOZZLE FLOW GRP | Address | 6 | 100% | 1% | 4 |
| 7 | PRANDTL MEYER FUNCTION | Author keyword | 6 | 100% | 1% | 4 |
| 8 | ALTITUDE COMPENSATION | Author keyword | 3 | 100% | 1% | 3 |
| 9 | CALORICALLY IMPERFECT GAS | Author keyword | 3 | 100% | 1% | 3 |
| 10 | OVER EXPANSION FLOW | Author keyword | 3 | 100% | 1% | 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 | RESTRICTED SHOCK SEPARATION | 38 | 93% | 3% | 14 | Search RESTRICTED+SHOCK+SEPARATION | Search RESTRICTED+SHOCK+SEPARATION |
| 2 | FREE SHOCK SEPARATION | 15 | 82% | 2% | 9 | Search FREE+SHOCK+SEPARATION | Search FREE+SHOCK+SEPARATION |
| 3 | SIDE LOADS | 13 | 67% | 3% | 12 | Search SIDE+LOADS | Search SIDE+LOADS |
| 4 | PRANDTL MEYER FUNCTION | 6 | 100% | 1% | 4 | Search PRANDTL+MEYER+FUNCTION | Search PRANDTL+MEYER+FUNCTION |
| 5 | ALTITUDE COMPENSATION | 3 | 100% | 1% | 3 | Search ALTITUDE+COMPENSATION | Search ALTITUDE+COMPENSATION |
| 6 | CALORICALLY IMPERFECT GAS | 3 | 100% | 1% | 3 | Search CALORICALLY+IMPERFECT+GAS | Search CALORICALLY+IMPERFECT+GAS |
| 7 | OVER EXPANSION FLOW | 3 | 100% | 1% | 3 | Search OVER+EXPANSION+FLOW | Search OVER+EXPANSION+FLOW |
| 8 | SKYLON | 3 | 45% | 1% | 5 | Search SKYLON | Search SKYLON |
| 9 | PLUG NOZZLE | 3 | 50% | 1% | 4 | Search PLUG+NOZZLE | Search PLUG+NOZZLE |
| 10 | ROCKET NOZZLE | 2 | 28% | 2% | 7 | Search ROCKET+NOZZLE | Search ROCKET+NOZZLE |
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 | RESTRICTED SHOCK SEPARATION | 27 | 83% | 4% | 15 |
| 2 | ROCKET NOZZLES | 16 | 65% | 4% | 15 |
| 3 | SIDE LOADS | 11 | 67% | 2% | 10 |
| 4 | CLUSTERED NOZZLE CONFIGURATION | 8 | 100% | 1% | 5 |
| 5 | OPTIMUM THRUST | 6 | 80% | 1% | 4 |
| 6 | ENGINE NOZZLE | 6 | 100% | 1% | 4 |
| 7 | FAST EULER SOLVER | 6 | 100% | 1% | 4 |
| 8 | OPTIMIZED PARABOLIC NOZZLE | 6 | 100% | 1% | 4 |
| 9 | SIDE LOAD ANALYSIS | 4 | 75% | 1% | 3 |
| 10 | CONTOUR NOZZLE | 2 | 67% | 0% | 2 |
Journals |
Reviews |
| Title | Publ. year | Cit. | Active references |
% act. ref. to same field |
|---|---|---|---|---|
| Inviscid and viscous flow computations by means of a lambda methodology: A review | 1997 | 0 | 12 | 58% |
| COMPUTATION OF FLOWS WITH SHOCKS | 1987 | 43 | 17 | 18% |
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 | PROP STRUCT THERMAL FLUIDS ANAL | 8 | 100% | 1.2% | 5 |
| 2 | LIQUID ENGINE MAIN PROP SYST BRANCH | 6 | 100% | 1.0% | 4 |
| 3 | NOZZLE FLOW GRP | 6 | 100% | 1.0% | 4 |
| 4 | PROP SYST DESIGN INTEGRAT | 3 | 100% | 0.7% | 3 |
| 5 | FLUID DYNAM BRANCH | 3 | 37% | 1.7% | 7 |
| 6 | DPTO PROGRAMAS ESPACIALES | 2 | 67% | 0.5% | 2 |
| 7 | PL FLUID DYNAM ANAL GRP | 2 | 50% | 0.7% | 3 |
| 8 | EXPT AERODYNAM | 2 | 17% | 2.7% | 11 |
| 9 | CULHAM SCI D5 | 1 | 38% | 0.7% | 3 |
| 10 | DIP MECCAN AERONAUT | 1 | 50% | 0.5% | 2 |
Related classes at same level (level 1) |
| Rank | Relatedness score | Related classes |
|---|---|---|
| 1 | 0.0000162530 | COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER |
| 2 | 0.0000126647 | HARTMANN WHISTLE//FLORIDA ADV AEROPROPULS//MACH DISK |
| 3 | 0.0000106383 | CARBUNCLE PHENOMENON//SHOCK INSTABILITY//MACH UNIFORM |
| 4 | 0.0000089878 | SHOCK VORTEX INTERACTION//BACKGROUND ORIENTED SCHLIEREN//COMPRESSIBLE VORTEX RING |
| 5 | 0.0000089169 | FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS |
| 6 | 0.0000088140 | SENSITIVITY EQUATION METHOD//CODE VERIFICATION//MANUFACTURED SOLUTIONS |
| 7 | 0.0000085019 | SCRAMJET//SUPERSONIC COMBUSTION//JOURNAL OF PROPULSION AND POWER |
| 8 | 0.0000075519 | TRANSONIC SHOCK//NONLINEAR WAVE SYSTEM//TRANSONIC SHOCKS |
| 9 | 0.0000067126 | LOCAL SUPERSONIC REGIONS//INVERSE DESIGN//AEROSP PROP GRP |
| 10 | 0.0000066926 | SPACE TOURISM//INT AIR SPACE LAW//SPACE LAW |