| 1552 different keywords | Search | Percent |
|---|
| cavitation | 512 | 7.9 % |
| of | 228 | 3.5 % |
| pdf | 113 | 1.7 % |
| in | 112 | 1.7 % |
| propeller | 104 | 1.6 % |
| and | 96 | 1.4 % |
| orifice | 93 | 1.4 % |
| pump | 89 | 1.3 % |
| the | 73 | 1.1 % |
| on | 69 | 1 % |
| bubble | 68 | 1 % |
| a | 67 | 1 % |
| flow | 64 | 0.9 % |
| fluent | 64 | 0.9 % |
| vortex | 58 | 0.9 % |
| numerical | 48 | 0.7 % |
| centrifugal | 47 | 0.7 % |
| filetype | 45 | 0.6 % |
| simulation | 44 | 0.6 % |
| water | 44 | 0.6 % |
| restriction | 42 | 0.6 % |
| pressure | 42 | 0.6 % |
| analysis | 42 | 0.6 % |
| model | 41 | 0.6 % |
| for | 39 | 0.6 % |
| cavitating | 36 | 0.5 % |
| jet | 31 | 0.4 % |
| bubbles | 28 | 0.4 % |
| pumps | 27 | 0.4 % |
| rudder | 26 | 0.4 % |
| turbine | 25 | 0.3 % |
| frequency | 25 | 0.3 % |
| unsteady | 24 | 0.3 % |
| to | 24 | 0.3 % |
| supercavitation | 24 | 0.3 % |
| noise | 24 | 0.3 % |
| ship | 22 | 0.3 % |
| flows | 21 | 0.3 % |
| propellers | 21 | 0.3 % |
| joint | 21 | 0.3 % |
| surface | 20 | 0.3 % |
| blade | 20 | 0.3 % |
| with | 20 | 0.3 % |
| cavity | 20 | 0.3 % |
| tunnel | 20 | 0.3 % |
| kaplan | 20 | 0.3 % |
| 2001 | 19 | 0.2 % |
| hydrofoil | 19 | 0.2 % |
| using | 19 | 0.2 % |
| method | 19 | 0.2 % |
| turbopump | 18 | 0.2 % |
| marine | 18 | 0.2 % |
| symposium | 18 | 0.2 % |
| angle | 18 | 0.2 % |
| design | 18 | 0.2 % |
| experimental | 18 | 0.2 % |
| erosion | 17 | 0.2 % |
| edge | 17 | 0.2 % |
| time | 17 | 0.2 % |
| modeling | 17 | 0.2 % |
| supercavitating | 16 | 0.2 % |
| inducer | 16 | 0.2 % |
| thesis | 16 | 0.2 % |
| test | 15 | 0.2 % |
| coefficient | 15 | 0.2 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 15 | 0.2 % |
| from | 15 | 0.2 % |
| leading | 15 | 0.2 % |
| piercing | 15 | 0.2 % |
| by | 14 | 0.2 % |
| dynamics | 14 | 0.2 % |
| study | 14 | 0.2 % |
| number | 14 | 0.2 % |
| collapse | 14 | 0.2 % |
| an | 14 | 0.2 % |
| cav2001 | 14 | 0.2 % |
| prediction | 14 | 0.2 % |
| cfd | 14 | 0.2 % |
| hydraulic | 14 | 0.2 % |
| video | 13 | 0.2 % |
| liquid | 13 | 0.2 % |
| diesel | 13 | 0.2 % |
| sheet | 13 | 0.2 % |
| nozzle | 13 | 0.2 % |
| calculation | 13 | 0.2 % |
| how | 12 | 0.1 % |
| is | 12 | 0.1 % |
| vibration | 12 | 0.1 % |
| dynamic | 12 | 0.1 % |
| detachment | 12 | 0.1 % |
| partial | 12 | 0.1 % |
| lattice | 12 | 0.1 % |
| effect | 12 | 0.1 % |
| at | 12 | 0.1 % |
| effects | 12 | 0.1 % |
| drag | 11 | 0.1 % |
| distribution | 11 | 0.1 % |
| hydrodynamic | 11 | 0.1 % |
| speed | 11 | 0.1 % |
| plate | 11 | 0.1 % |
| international | 11 | 0.1 % |
| valve | 11 | 0.1 % |
| near | 11 | 0.1 % |
| experiment | 10 | 0.1 % |
| type | 10 | 0.1 % |
| behavior | 10 | 0.1 % |
| rocket | 10 | 0.1 % |
| damage | 10 | 0.1 % |
| between | 10 | 0.1 % |
| re-entrant | 10 | 0.1 % |
| m. | 10 | 0.1 % |
| equation | 10 | 0.1 % |
| turbo | 10 | 0.1 % |
| inception | 10 | 0.1 % |
| high | 10 | 0.1 % |
| what | 9 | 0.1 % |
| fluid | 9 | 0.1 % |
| pipe | 9 | 0.1 % |
| acoustic | 9 | 0.1 % |
| turbines | 9 | 0.1 % |
| tip | 9 | 0.1 % |
| time-frequency | 9 | 0.1 % |
| boundary | 9 | 0.1 % |
| wave | 9 | 0.1 % |
| cavities | 9 | 0.1 % |
| cav | 9 | 0.1 % |
| suction | 9 | 0.1 % |
| luminescence | 9 | 0.1 % |
| spectrum | 9 | 0.1 % |
| phase | 8 | 0.1 % |
| instability | 8 | 0.1 % |
| artificial | 8 | 0.1 % |
| vof | 8 | 0.1 % |
| & | 8 | 0.1 % |
| reentrant | 8 | 0.1 % |
| based | 8 | 0.1 % |
| ventilated | 8 | 0.1 % |
| kinnas | 8 | 0.1 % |
| types | 8 | 0.1 % |
| tab_hty | 8 | 0.1 % |
| shock | 8 | 0.1 % |
| characteristics | 8 | 0.1 % |
| orifices | 8 | 0.1 % |
| song | 8 | 0.1 % |
| submerged | 8 | 0.1 % |
| caltech | 7 | 0.1 % |
| injector | 7 | 0.1 % |
| ratio | 7 | 0.1 % |
| pitch | 7 | 0.1 % |
| point | 7 | 0.1 % |
| butterfly | 7 | 0.1 % |
| velocity | 7 | 0.1 % |
| or | 7 | 0.1 % |
| naca | 7 | 0.1 % |
| approach | 7 | 0.1 % |
| cloud | 7 | 0.1 % |
| turbulence | 7 | 0.1 % |
| modelling | 7 | 0.1 % |
| charles | 6 | 0 % |
| 4th | 6 | 0 % |
| viscosity | 6 | 0 % |
| mass | 6 | 0 % |
| scale | 6 | 0 % |
| sound | 6 | 0 % |
| paper | 6 | 0 % |
| cascade | 6 | 0 % |
| g. | 6 | 0 % |
| free | 6 | 0 % |
| measurements | 6 | 0 % |
| investigations | 6 | 0 % |
| turbomachinery | 6 | 0 % |
| code | 6 | 0 % |
| j. | 6 | 0 % |
| impeller | 6 | 0 % |
| spherical | 6 | 0 % |
| boncinelli | 6 | 0 % |
| problems | 6 | 0 % |
| laser-induced | 6 | 0 % |
| side | 6 | 0 % |
| methods | 6 | 0 % |
| .pdf | 6 | 0 % |
| paolo | 6 | 0 % |
| validation | 6 | 0 % |
| semenov | 6 | 0 % |
| serebryakov | 5 | 0 % |
| measurement | 5 | 0 % |
| author | 5 | 0 % |
| azipod | 5 | 0 % |
| yuriy | 5 | 0 % |
| correlation | 5 | 0 % |
| equations | 5 | 0 % |
| journal | 5 | 0 % |
| b. | 5 | 0 % |
| models | 5 | 0 % |
| de | 5 | 0 % |
| performance | 5 | 0 % |
| over | 5 | 0 % |
| astm | 5 | 0 % |
| ventilation | 5 | 0 % |
| surface-piercing | 5 | 0 % |
| oil | 5 | 0 % |
| inducers | 5 | 0 % |
| engine | 5 | 0 % |
| disk | 5 | 0 % |
| . | 5 | 0 % |
| npsh | 5 | 0 % |
| reduction | 5 | 0 % |
| c.s. | 5 | 0 % |
| injection | 5 | 0 % |
| bem | 5 | 0 % |
| discharge | 5 | 0 % |
| difference | 5 | 0 % |
| hosangadi | 5 | 0 % |
| cryogenic | 5 | 0 % |
| single | 5 | 0 % |
| kosyna | 5 | 0 % |
| critical | 5 | 0 % |
| balance | 5 | 0 % |
| volume | 5 | 0 % |
| gas | 5 | 0 % |
| investigation | 5 | 0 % |
| head | 5 | 0 % |
| keller | 5 | 0 % |
| site | 5 | 0 % |
| material | 5 | 0 % |
| underwater | 4 | 0 % |
| shockwave | 4 | 0 % |
| nucleation | 4 | 0 % |
| problem | 4 | 0 % |
| inlet | 4 | 0 % |
| rate | 4 | 0 % |
| change | 4 | 0 % |
| implicit | 4 | 0 % |
| causes | 4 | 0 % |
| laser | 4 | 0 % |
| state | 4 | 0 % |
| j | 4 | 0 % |
| step | 4 | 0 % |
| about | 4 | 0 % |
| algorithm | 4 | 0 % |
| axial | 4 | 0 % |
| oscillations | 4 | 0 % |
| 1987 | 4 | 0 % |
| bodies | 4 | 0 % |
| cone | 4 | 0 % |
| hull | 4 | 0 % |
| dimensional | 4 | 0 % |
| length | 4 | 0 % |
| cavitator | 4 | 0 % |
| stokes | 4 | 0 % |
| restricted | 4 | 0 % |
| foil | 4 | 0 % |
| distance | 4 | 0 % |
| molecular | 4 | 0 % |
| surge | 4 | 0 % |
| layer | 4 | 0 % |
| transfer | 4 | 0 % |
| strenght | 4 | 0 % |
| merkle | 4 | 0 % |
| atlar | 4 | 0 % |
| arndt | 4 | 0 % |
| caviling | 4 | 0 % |
| theory | 4 | 0 % |
| inside | 4 | 0 % |
| 3d | 4 | 0 % |
| boundaries | 4 | 0 % |
| technology | 4 | 0 % |
| diagram | 4 | 0 % |
| size | 4 | 0 % |
| new | 4 | 0 % |
| three | 4 | 0 % |
| collapsing | 4 | 0 % |
| simulations | 4 | 0 % |
| stoffel | 4 | 0 % |
| .edu | 4 | 0 % |
| lamp | 4 | 0 % |
| schnerr | 4 | 0 % |
| induced | 4 | 0 % |
| avellan | 4 | 0 % |
| rig | 4 | 0 % |
| farhat | 4 | 0 % |
| potential | 4 | 0 % |
| phd | 4 | 0 % |
| level | 4 | 0 % |
| supercavity | 4 | 0 % |
| efficiency | 4 | 0 % |
| ships | 4 | 0 % |
| michel | 4 | 0 % |
| calculate | 4 | 0 % |
| nexearch | 4 | 0 % |
| air | 4 | 0 % |
| rigid | 3 | 0 % |
| horn | 3 | 0 % |
| wall | 3 | 0 % |
| fraction | 3 | 0 % |
| jets | 3 | 0 % |
| prop | 3 | 0 % |
| star-cd | 3 | 0 % |
| kubota | 3 | 0 % |
| sauer | 3 | 0 % |
| static | 3 | 0 % |
| national | 3 | 0 % |
| navier-stokes | 3 | 0 % |
| perspectives | 3 | 0 % |
| kam | 3 | 0 % |
| piping | 3 | 0 % |
| density | 3 | 0 % |
| hydrauliques | 3 | 0 % |
| conditions | 3 | 0 % |
| tsujimoto | 3 | 0 % |
| intake | 3 | 0 % |
| 1 | 3 | 0 % |
| r. | 3 | 0 % |
| liquids | 3 | 0 % |
| hoffman | 3 | 0 % |
| oxygen | 3 | 0 % |
| emission | 3 | 0 % |
| radius | 3 | 0 % |
| normal | 3 | 0 % |
| technical | 3 | 0 % |
| injectors | 3 | 0 % |
| due | 3 | 0 % |
| soyama | 3 | 0 % |
| introduction | 3 | 0 % |
| small | 3 | 0 % |
| savchenko | 3 | 0 % |
| panel | 3 | 0 % |
| [pdf] | 3 | 0 % |
| ng | 3 | 0 % |
| past | 3 | 0 % |
| webkr | 3 | 0 % |
| propellor | 3 | 0 % |
| through | 3 | 0 % |
| okada | 3 | 0 % |
| developed | 3 | 0 % |
| added | 3 | 0 % |
| channel | 3 | 0 % |
| spectrometer | 3 | 0 % |
| frv | 3 | 0 % |
| large | 3 | 0 % |
| lithotripsy | 3 | 0 % |
| elrod | 3 | 0 % |
| compressible | 3 | 0 % |
| solve | 3 | 0 % |
| interaction | 3 | 0 % |
| research | 3 | 0 % |
| working | 3 | 0 % |
| podded | 3 | 0 % |
| turbulent | 3 | 0 % |
| comparison | 3 | 0 % |
| vladimir | 3 | 0 % |
| “similarities | 3 | 0 % |
| cylindrical | 3 | 0 % |
| - | 3 | 0 % |
| fft | 3 | 0 % |
| turbopumps | 3 | 0 % |
| les | 3 | 0 % |
| systems | 3 | 0 % |
| multiphase | 3 | 0 % |
| single-phase | 3 | 0 % |
| 0015 | 3 | 0 % |
| development | 3 | 0 % |
| kunz | 3 | 0 % |
| ukraine | 3 | 0 % |
| control | 3 | 0 % |
| pattern | 3 | 0 % |
| entry | 3 | 0 % |
| ultrasound | 3 | 0 % |
| geometrical | 3 | 0 % |
| abs | 3 | 0 % |
| element | 3 | 0 % |
| section | 3 | 0 % |
| hole | 3 | 0 % |
| signal | 3 | 0 % |
| chen | 3 | 0 % |
| a8.004. | 3 | 0 % |
| maeda | 3 | 0 % |
| et | 3 | 0 % |
| compressibility | 3 | 0 % |
| university | 3 | 0 % |
| results | 3 | 0 % |
| – | 3 | 0 % |
| steel | 3 | 0 % |
| temperature | 3 | 0 % |
| curvature | 3 | 0 % |
| friedrichs | 3 | 0 % |
| drawing | 3 | 0 % |
| hitoshi | 3 | 0 % |
| forces | 3 | 0 % |
| navier | 3 | 0 % |
| thrust | 3 | 0 % |
| points | 3 | 0 % |
| 2 | 3 | 0 % |
| bubbly | 3 | 0 % |
| g134 | 3 | 0 % |
| boat | 3 | 0 % |
| rarefaction | 3 | 0 % |
| wear | 3 | 0 % |
| coordinates | 3 | 0 % |
| plesset | 3 | 0 % |
| outlet | 3 | 0 % |
| session | 3 | 0 % |
| characteristic | 3 | 0 % |
| franc | 3 | 0 % |
| find | 3 | 0 % |
| root | 3 | 0 % |
| homogeneous | 3 | 0 % |
| robert | 3 | 0 % |
| onr | 3 | 0 % |
| laboratory | 3 | 0 % |
| kuklinski | 3 | 0 % |
| rayleigh | 3 | 0 % |
| h | 3 | 0 % |
| studies | 3 | 0 % |
| cluster | 3 | 0 % |
| multi | 3 | 0 % |
| form | 2 | 0 % |
| closure | 2 | 0 % |
| iwai | 2 | 0 % |
| projectile | 2 | 0 % |
| controllable | 2 | 0 % |
| finite | 2 | 0 % |
| aerofoils | 2 | 0 % |
| method. | 2 | 0 % |
| shapes | 2 | 0 % |
| m/s | 2 | 0 % |
| aiaa | 2 | 0 % |
| equilibrium | 2 | 0 % |
| energy | 2 | 0 % |
| tomita | 2 | 0 % |
| analyser | 2 | 0 % |
| will | 2 | 0 % |
| bernoulli | 2 | 0 % |
| super | 2 | 0 % |
| exact | 2 | 0 % |
| nonspherical | 2 | 0 % |
| can | 2 | 0 % |
| yoshinobu | 2 | 0 % |
| virtual | 2 | 0 % |
| lab | 2 | 0 % |
| t. | 2 | 0 % |
| qian | 2 | 0 % |
| g.h. | 2 | 0 % |
| k | 2 | 0 % |
| cause | 2 | 0 % |
| plates | 2 | 0 % |
| y-savchenko | 2 | 0 % |
| converging | 2 | 0 % |
| computational | 2 | 0 % |
| laser-created | 2 | 0 % |
| runner | 2 | 0 % |
| terms | 2 | 0 % |
| stainless | 2 | 0 % |
| mech. | 2 | 0 % |
| grid | 2 | 0 % |
| c. | 2 | 0 % |
| ductile | 2 | 0 % |
| heat | 2 | 0 % |
| software | 2 | 0 % |
| kamijo | 2 | 0 % |
| solid | 2 | 0 % |
| transducer | 2 | 0 % |
| p=cte | 2 | 0 % |
| producing | 2 | 0 % |
| explosion | 2 | 0 % |
| vapor | 2 | 0 % |
| int | 2 | 0 % |
| forairfoil | 2 | 0 % |
| measuring | 2 | 0 % |
| sg4 | 2 | 0 % |
| making | 2 | 0 % |
| shf | 2 | 0 % |
| institute | 2 | 0 % |
| pressures | 2 | 0 % |
| fluctuations | 2 | 0 % |
| inter | 2 | 0 % |
| ccs | 2 | 0 % |
| rayleigh-plesset | 2 | 0 % |
| propulsors | 2 | 0 % |
| bell | 2 | 0 % |
| effects-empirically | 2 | 0 % |
| relation | 2 | 0 % |
| chart | 2 | 0 % |
| 1975 | 2 | 0 % |
| wing | 2 | 0 % |
| convergent-divergent | 2 | 0 % |
| shen | 2 | 0 % |
| speeds | 2 | 0 % |
| p | 2 | 0 % |
| oscillation | 2 | 0 % |
| shaping | 2 | 0 % |
| relations | 2 | 0 % |
| file | 2 | 0 % |
| y | 2 | 0 % |
| naca66 | 2 | 0 % |
| fine | 2 | 0 % |
| aggressiveness | 2 | 0 % |
| ch4 | 2 | 0 % |
| regiane | 2 | 0 % |
| tissue | 2 | 0 % |
| vibrations | 2 | 0 % |
| delgosha | 2 | 0 % |
| found | 2 | 0 % |
| patella | 2 | 0 % |
| pipes | 2 | 0 % |
| gb | 2 | 0 % |
| fluids | 2 | 0 % |
| tips | 2 | 0 % |
| calculating | 2 | 0 % |
| oti | 2 | 0 % |
| semi | 2 | 0 % |
| 1995 | 2 | 0 % |
| rotating | 2 | 0 % |
| impact | 2 | 0 % |
| papers | 2 | 0 % |
| low | 2 | 0 % |
| fluctuation | 2 | 0 % |
| impulsive | 2 | 0 % |
| table | 2 | 0 % |
| jsme | 2 | 0 % |
| observations | 2 | 0 % |
| b | 2 | 0 % |
| wiki | 2 | 0 % |
| ap | 2 | 0 % |
| function | 2 | 0 % |
| streamline | 2 | 0 % |
| born | 2 | 0 % |
| sizing | 2 | 0 % |
| face | 2 | 0 % |
| solution | 2 | 0 % |
| sae | 2 | 0 % |
| motion | 2 | 0 % |
| aspects | 2 | 0 % |
| vogel | 2 | 0 % |
| techniques | 2 | 0 % |
| improvement | 2 | 0 % |
| david | 2 | 0 % |
| brennen | 2 | 0 % |
| 40 | 2 | 0 % |
| process | 2 | 0 % |
| s. | 2 | 0 % |
| reynolds | 2 | 0 % |
| boundaries. | 2 | 0 % |
| solutions | 2 | 0 % |
| fortes-patella | 2 | 0 % |
| survey | 2 | 0 % |
| tullis | 2 | 0 % |
| physical | 2 | 0 % |
| breakdown | 2 | 0 % |
| example | 2 | 0 % |
| force | 2 | 0 % |
| additives | 2 | 0 % |
| phenomenon | 2 | 0 % |
| hh | 2 | 0 % |
| wedge-shaped | 2 | 0 % |
| strouhal | 2 | 0 % |
| program | 2 | 0 % |
| power | 2 | 0 % |
| history | 2 | 0 % |
| y. | 2 | 0 % |
| zero | 2 | 0 % |
| generation | 2 | 0 % |
| transients | 2 | 0 % |
| photography | 2 | 0 % |
| mixture | 2 | 0 % |
| review | 2 | 0 % |
| chord | 2 | 0 % |
| sanchez | 2 | 0 % |
| tank | 2 | 0 % |
| geometry | 2 | 0 % |
| piv | 2 | 0 % |
| jean | 2 | 0 % |
| hart | 2 | 0 % |
| schnerr. | 2 | 0 % |
| iterative | 2 | 0 % |
| factor | 2 | 0 % |
| mechanisms | 2 | 0 % |
| erosive | 2 | 0 % |
| cp | 2 | 0 % |
| as | 2 | 0 % |
| hattori shuji 1985 | 2 | 0 % |
| why | 2 | 0 % |
| 5 | 2 | 0 % |
| ryabushinsky | 2 | 0 % |
| has | 2 | 0 % |
| kato | 2 | 0 % |
| g32-92 | 2 | 0 % |
| day | 2 | 0 % |
| maneuvering | 2 | 0 % |
| engineering | 2 | 0 % |
| behaviour | 2 | 0 % |
| modified | 2 | 0 % |
| 1997 | 2 | 0 % |
| negative | 2 | 0 % |
| tanguay | 2 | 0 % |
| kvaerner | 2 | 0 % |
| doublet | 2 | 0 % |
| physics | 2 | 0 % |
| production | 2 | 0 % |
| occasion | 2 | 0 % |
| ser | 2 | 0 % |
| japikse | 2 | 0 % |
| during | 2 | 0 % |
| heister | 2 | 0 % |
| meter | 2 | 0 % |
| multiple | 2 | 0 % |
| technologies | 2 | 0 % |
| street | 2 | 0 % |
| chahine | 2 | 0 % |
| gap | 2 | 0 % |
| yamaguchi | 2 | 0 % |
| t | 2 | 0 % |
| evaluation | 2 | 0 % |
| burst | 2 | 0 % |
| asce | 2 | 0 % |
| downstream | 2 | 0 % |
| blake | 2 | 0 % |
| s55c | 2 | 0 % |
| transient | 2 | 0 % |
| c-lee | 2 | 0 % |
| venturi | 2 | 0 % |
| fourth | 2 | 0 % |
| francis | 2 | 0 % |
| vapour | 2 | 0 % |
| tests | 2 | 0 % |
| eulerian/lagrangian | 2 | 0 % |
| literature | 2 | 0 % |
| hofmann | 2 | 0 % |
| conclusion | 2 | 0 % |
| two | 2 | 0 % |
| viscous | 2 | 0 % |
| diverging | 2 | 0 % |
| lubrication | 2 | 0 % |
| airfoil | 2 | 0 % |
| formation | 2 | 0 % |
| inverse | 2 | 0 % |
| multielement | 2 | 0 % |
| tube | 2 | 0 % |
| technique | 2 | 0 % |
| torque | 2 | 0 % |
| w. | 2 | 0 % |
| 2009 | 2 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 2 | 0 % |
| radial | 2 | 0 % |
| plot | 2 | 0 % |
| probing | 2 | 0 % |
| mixed | 2 | 0 % |
| yuan | 2 | 0 % |
| predict | 2 | 0 % |
| a. | 2 | 0 % |
| c61 | 2 | 0 % |
| zhang | 2 | 0 % |
| criteria | 2 | 0 % |
| fission | 2 | 0 % |
| clouds | 2 | 0 % |
| flanges | 2 | 0 % |
| lauterborn | 2 | 0 % |
| collapses | 2 | 0 % |
| works | 2 | 0 % |
| parsons | 2 | 0 % |
| penn | 2 | 0 % |
| hydrophone | 2 | 0 % |
| testing | 2 | 0 % |
| phenomena | 2 | 0 % |
| micro | 2 | 0 % |
| condensation | 2 | 0 % |
| experience | 2 | 0 % |
| ball | 2 | 0 % |
| 2d | 2 | 0 % |
| mixing | 2 | 0 % |
| one | 2 | 0 % |
| v. | 2 | 0 % |
| installation | 2 | 0 % |
| dissipator | 2 | 0 % |
| r.f. | 2 | 0 % |
| 3rd | 2 | 0 % |
| dj@conceptsnrec.com | 2 | 0 % |
| lecoffre | 2 | 0 % |
| three-dimensionality | 2 | 0 % |
| mid-chord | 2 | 0 % |
| high-speed | 2 | 0 % |
| hammer | 2 | 0 % |
| 1998 | 2 | 0 % |
| abstract | 2 | 0 % |
| advance | 2 | 0 % |
| world | 2 | 0 % |
| passenger | 2 | 0 % |
| straight | 2 | 0 % |
| barotropic | 2 | 0 % |
| polymers | 2 | 0 % |
| f | 2 | 0 % |
| epfl | 2 | 0 % |
| tokyo | 2 | 0 % |
| first | 2 | 0 % |
| hjim | 2 | 0 % |
| lacombe | 2 | 0 % |
| structure | 2 | 0 % |
| murtuza | 1 | 0 % |
| n. | 1 | 0 % |
| d.c. | 1 | 0 % |
| particle | 1 | 0 % |
| rotation | 1 | 0 % |
| n-s | 1 | 0 % |
| excessive | 1 | 0 % |
| light | 1 | 0 % |
| pitting | 1 | 0 % |
| cryostat | 1 | 0 % |
| counterjet | 1 | 0 % |
| kirschner | 1 | 0 % |
| disadvantages | 1 | 0 % |
| direction | 1 | 0 % |
| developments | 1 | 0 % |
| sumulations | 1 | 0 % |
| procedure | 1 | 0 % |
| command | 1 | 0 % |
| vessels | 1 | 0 % |
| part | 1 | 0 % |
| kaplan´s | 1 | 0 % |
| prads | 1 | 0 % |
| zur | 1 | 0 % |
| sv402 | 1 | 0 % |
| cores | 1 | 0 % |
| where | 1 | 0 % |
| choked | 1 | 0 % |
| nasa | 1 | 0 % |
| spalart-allmaras | 1 | 0 % |
| takeshi | 1 | 0 % |
| dang | 1 | 0 % |
| hydrogen | 1 | 0 % |
| bolle | 1 | 0 % |
| sample | 1 | 0 % |
| visual | 1 | 0 % |
| setting | 1 | 0 % |
| astern | 1 | 0 % |
| vertical | 1 | 0 % |
| 2-d | 1 | 0 % |
| indexes | 1 | 0 % |
| venkateswaran | 1 | 0 % |
| project | 1 | 0 % |
| hv | 1 | 0 % |
| mechanics | 1 | 0 % |
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