| 1507 different keywords | Search | Percent |
|---|
| cavitation | 443 | 6.8 % |
| of | 274 | 4.2 % |
| pdf | 132 | 2 % |
| in | 105 | 1.6 % |
| orifice | 101 | 1.5 % |
| pump | 94 | 1.4 % |
| propeller | 90 | 1.3 % |
| and | 84 | 1.2 % |
| flow | 81 | 1.2 % |
| the | 78 | 1.2 % |
| bubble | 68 | 1 % |
| a | 67 | 1 % |
| filetype | 64 | 0.9 % |
| on | 63 | 0.9 % |
| vortex | 59 | 0.9 % |
| water | 53 | 0.8 % |
| restriction | 52 | 0.8 % |
| centrifugal | 50 | 0.7 % |
| fluent | 45 | 0.6 % |
| noise | 38 | 0.5 % |
| erosion | 34 | 0.5 % |
| hydrofoil | 34 | 0.5 % |
| supercavitating | 34 | 0.5 % |
| method | 34 | 0.5 % |
| for | 34 | 0.5 % |
| numerical | 33 | 0.5 % |
| model | 33 | 0.5 % |
| design | 33 | 0.5 % |
| pressure | 32 | 0.4 % |
| analysis | 32 | 0.4 % |
| supercavitation | 32 | 0.4 % |
| propellers | 31 | 0.4 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 31 | 0.4 % |
| cavitating | 30 | 0.4 % |
| surface | 29 | 0.4 % |
| to | 29 | 0.4 % |
| ship | 29 | 0.4 % |
| rudder | 28 | 0.4 % |
| pumps | 27 | 0.4 % |
| inducer | 26 | 0.4 % |
| simulation | 26 | 0.4 % |
| unsteady | 23 | 0.3 % |
| an | 23 | 0.3 % |
| by | 22 | 0.3 % |
| with | 21 | 0.3 % |
| cav2001 | 21 | 0.3 % |
| frequency | 20 | 0.3 % |
| kaplan | 20 | 0.3 % |
| experimental | 20 | 0.3 % |
| number | 19 | 0.2 % |
| collapse | 19 | 0.2 % |
| tip | 19 | 0.2 % |
| cavity | 19 | 0.2 % |
| sheet | 19 | 0.2 % |
| jet | 18 | 0.2 % |
| flows | 18 | 0.2 % |
| boundary | 18 | 0.2 % |
| equation | 18 | 0.2 % |
| cfd | 18 | 0.2 % |
| pipe | 17 | 0.2 % |
| naca | 17 | 0.2 % |
| plate | 17 | 0.2 % |
| modelling | 17 | 0.2 % |
| azipod | 16 | 0.2 % |
| how | 16 | 0.2 % |
| blade | 16 | 0.2 % |
| joint | 16 | 0.2 % |
| experiment | 15 | 0.2 % |
| bubbles | 15 | 0.2 % |
| types | 15 | 0.2 % |
| orifices | 15 | 0.2 % |
| calculation | 15 | 0.2 % |
| study | 14 | 0.2 % |
| acoustic | 14 | 0.2 % |
| thesis | 14 | 0.2 % |
| characteristics | 14 | 0.2 % |
| effect | 14 | 0.2 % |
| test | 13 | 0.2 % |
| turbine | 13 | 0.2 % |
| rocket | 13 | 0.2 % |
| speed | 13 | 0.2 % |
| tunnel | 13 | 0.2 % |
| leading | 13 | 0.2 % |
| effects | 13 | 0.2 % |
| horn | 12 | 0.1 % |
| dynamics | 12 | 0.1 % |
| coefficient | 12 | 0.1 % |
| cavitator | 12 | 0.1 % |
| edge | 12 | 0.1 % |
| modeling | 12 | 0.1 % |
| kunz | 12 | 0.1 % |
| using | 12 | 0.1 % |
| submerged | 12 | 0.1 % |
| marine | 11 | 0.1 % |
| bodies | 11 | 0.1 % |
| or | 11 | 0.1 % |
| cloud | 11 | 0.1 % |
| suction | 11 | 0.1 % |
| video | 10 | 0.1 % |
| journal | 10 | 0.1 % |
| performance | 10 | 0.1 % |
| panel | 10 | 0.1 % |
| is | 10 | 0.1 % |
| ventilated | 10 | 0.1 % |
| impeller | 10 | 0.1 % |
| cavities | 10 | 0.1 % |
| prediction | 10 | 0.1 % |
| piercing | 10 | 0.1 % |
| observation | 9 | 0.1 % |
| reentrant | 9 | 0.1 % |
| distribution | 9 | 0.1 % |
| motion | 9 | 0.1 % |
| turbomachinery | 9 | 0.1 % |
| time | 9 | 0.1 % |
| control | 9 | 0.1 % |
| tab_hty | 9 | 0.1 % |
| wave | 9 | 0.1 % |
| formation | 9 | 0.1 % |
| gas | 9 | 0.1 % |
| japan | 9 | 0.1 % |
| hydraulic | 9 | 0.1 % |
| spectrum | 9 | 0.1 % |
| nozzle | 9 | 0.1 % |
| underwater | 8 | 0.1 % |
| turbopump | 8 | 0.1 % |
| axial | 8 | 0.1 % |
| formed | 8 | 0.1 % |
| 2001 | 8 | 0.1 % |
| rotating | 8 | 0.1 % |
| impact | 8 | 0.1 % |
| time-frequency | 8 | 0.1 % |
| vibration | 8 | 0.1 % |
| international | 8 | 0.1 % |
| problems | 8 | 0.1 % |
| diesel | 8 | 0.1 % |
| around | 8 | 0.1 % |
| 2d | 8 | 0.1 % |
| ships | 8 | 0.1 % |
| what | 7 | 0.1 % |
| symposium | 7 | 0.1 % |
| instability | 7 | 0.1 % |
| formula | 7 | 0.1 % |
| paper | 7 | 0.1 % |
| hydrodynamic | 7 | 0.1 % |
| velocity | 7 | 0.1 % |
| vessel | 7 | 0.1 % |
| 3d | 7 | 0.1 % |
| - | 7 | 0.1 % |
| resistance | 7 | 0.1 % |
| 0015 | 7 | 0.1 % |
| mechanism | 7 | 0.1 % |
| element | 7 | 0.1 % |
| size | 7 | 0.1 % |
| conference | 7 | 0.1 % |
| turbo | 7 | 0.1 % |
| 2 | 7 | 0.1 % |
| valve | 7 | 0.1 % |
| condition | 7 | 0.1 % |
| supercavity | 7 | 0.1 % |
| from | 7 | 0.1 % |
| site | 7 | 0.1 % |
| high | 7 | 0.1 % |
| air | 7 | 0.1 % |
| measurement | 6 | 0 % |
| wall | 6 | 0 % |
| phase | 6 | 0 % |
| fluid | 6 | 0 % |
| tsujimoto | 6 | 0 % |
| intake | 6 | 0 % |
| laser | 6 | 0 % |
| supersonic | 6 | 0 % |
| emission | 6 | 0 % |
| behavior | 6 | 0 % |
| injectors | 6 | 0 % |
| over | 6 | 0 % |
| quality | 6 | 0 % |
| oscillating | 6 | 0 % |
| butterfly | 6 | 0 % |
| through | 6 | 0 % |
| some | 6 | 0 % |
| shape | 6 | 0 % |
| damage | 6 | 0 % |
| tullis | 6 | 0 % |
| pictures | 6 | 0 % |
| numeca | 6 | 0 % |
| ross | 6 | 0 % |
| behind | 6 | 0 % |
| 1976 | 6 | 0 % |
| methods | 6 | 0 % |
| investigation | 6 | 0 % |
| luminescence | 6 | 0 % |
| cavitations | 6 | 0 % |
| keller | 6 | 0 % |
| structure | 6 | 0 % |
| system | 5 | 0 % |
| author | 5 | 0 % |
| change | 5 | 0 % |
| piping | 5 | 0 % |
| state | 5 | 0 % |
| artificial | 5 | 0 % |
| nuclei | 5 | 0 % |
| scale | 5 | 0 % |
| liquid | 5 | 0 % |
| sound | 5 | 0 % |
| hull | 5 | 0 % |
| criterion | 5 | 0 % |
| free | 5 | 0 % |
| company | 5 | 0 % |
| based | 5 | 0 % |
| observations | 5 | 0 % |
| b | 5 | 0 % |
| bearing | 5 | 0 % |
| wake | 5 | 0 % |
| engine | 5 | 0 % |
| between | 5 | 0 % |
| experiments | 5 | 0 % |
| injection | 5 | 0 % |
| multiphase | 5 | 0 % |
| d | 5 | 0 % |
| discharge | 5 | 0 % |
| sections | 5 | 0 % |
| meter | 5 | 0 % |
| volume | 5 | 0 % |
| turbulence | 5 | 0 % |
| two | 5 | 0 % |
| generated | 5 | 0 % |
| head | 5 | 0 % |
| induced | 5 | 0 % |
| s | 5 | 0 % |
| rarefaction | 5 | 0 % |
| vehicle | 5 | 0 % |
| high-speed | 5 | 0 % |
| at | 5 | 0 % |
| part | 4 | 0 % |
| 1999 | 4 | 0 % |
| computational | 4 | 0 % |
| solid | 4 | 0 % |
| equations | 4 | 0 % |
| drag | 4 | 0 % |
| injector | 4 | 0 % |
| series | 4 | 0 % |
| influence | 4 | 0 % |
| mass | 4 | 0 % |
| ltd | 4 | 0 % |
| vof | 4 | 0 % |
| intitle | 4 | 0 % |
| denshi | 4 | 0 % |
| stokes | 4 | 0 % |
| restricting | 4 | 0 % |
| asme | 4 | 0 % |
| turbines | 4 | 0 % |
| inducers | 4 | 0 % |
| layer | 4 | 0 % |
| sizing | 4 | 0 % |
| 1994 | 4 | 0 % |
| angle | 4 | 0 % |
| merkle | 4 | 0 % |
| field | 4 | 0 % |
| s. | 4 | 0 % |
| compressible | 4 | 0 % |
| inside | 4 | 0 % |
| phenomenon | 4 | 0 % |
| strouhal | 4 | 0 % |
| turbulent | 4 | 0 % |
| j. | 4 | 0 % |
| generation | 4 | 0 % |
| stability | 4 | 0 % |
| diagram | 4 | 0 % |
| two-dimensional | 4 | 0 % |
| data | 4 | 0 % |
| exhaust | 4 | 0 % |
| spherical | 4 | 0 % |
| boncinelli | 4 | 0 % |
| ultrasound | 4 | 0 % |
| engineering | 4 | 0 % |
| stage | 4 | 0 % |
| shock | 4 | 0 % |
| ppt | 4 | 0 % |
| approach | 4 | 0 % |
| new | 4 | 0 % |
| collapsing | 4 | 0 % |
| .pdf | 4 | 0 % |
| blades | 4 | 0 % |
| university | 4 | 0 % |
| paolo | 4 | 0 % |
| burrill | 4 | 0 % |
| airfoil | 4 | 0 % |
| three-dimensional | 4 | 0 % |
| temperature | 4 | 0 % |
| clearance | 4 | 0 % |
| mixed | 4 | 0 % |
| cav | 4 | 0 % |
| plesset | 4 | 0 % |
| potential | 4 | 0 % |
| riken | 4 | 0 % |
| minimum | 4 | 0 % |
| sea | 4 | 0 % |
| song | 4 | 0 % |
| abstract | 4 | 0 % |
| inception | 4 | 0 % |
| rayleigh | 4 | 0 % |
| first | 4 | 0 % |
| diameter | 4 | 0 % |
| nexearch | 4 | 0 % |
| multi | 4 | 0 % |
| finite | 3 | 0 % |
| equilibrium | 3 | 0 % |
| energy | 3 | 0 % |
| 4th | 3 | 0 % |
| super | 3 | 0 % |
| helical | 3 | 0 % |
| plates | 3 | 0 % |
| type | 3 | 0 % |
| trailing | 3 | 0 % |
| grid | 3 | 0 % |
| avoid | 3 | 0 % |
| heat | 3 | 0 % |
| vortices | 3 | 0 % |
| vapor | 3 | 0 % |
| density | 3 | 0 % |
| hydrauliques | 3 | 0 % |
| naca0015 | 3 | 0 % |
| ratio | 3 | 0 % |
| compressor | 3 | 0 % |
| thickness | 3 | 0 % |
| occurs | 3 | 0 % |
| step | 3 | 0 % |
| about | 3 | 0 % |
| john | 3 | 0 % |
| parameter | 3 | 0 % |
| wing | 3 | 0 % |
| facilities | 3 | 0 % |
| & | 3 | 0 % |
| bar | 3 | 0 % |
| download | 3 | 0 % |
| small | 3 | 0 % |
| cascade | 3 | 0 % |
| length | 3 | 0 % |
| index | 3 | 0 % |
| hydrofoils | 3 | 0 % |
| foil | 3 | 0 % |
| distance | 3 | 0 % |
| bernd | 3 | 0 % |
| breakoff | 3 | 0 % |
| jsme | 3 | 0 % |
| applied | 3 | 0 % |
| solution | 3 | 0 % |
| sae | 3 | 0 % |
| camera | 3 | 0 % |
| david | 3 | 0 % |
| fortes | 3 | 0 % |
| v | 3 | 0 % |
| theory | 3 | 0 % |
| solver | 3 | 0 % |
| research | 3 | 0 % |
| are | 3 | 0 % |
| . | 3 | 0 % |
| physical | 3 | 0 % |
| application | 3 | 0 % |
| power | 3 | 0 % |
| waves | 3 | 0 % |
| reduction | 3 | 0 % |
| comparison | 3 | 0 % |
| steady | 3 | 0 % |
| piv | 3 | 0 % |
| development | 3 | 0 % |
| circulation | 3 | 0 % |
| tait | 3 | 0 % |
| 5 | 3 | 0 % |
| entry | 3 | 0 % |
| applications | 3 | 0 % |
| abs | 3 | 0 % |
| 1997 | 3 | 0 % |
| section | 3 | 0 % |
| body | 3 | 0 % |
| swirl | 3 | 0 % |
| internal | 3 | 0 % |
| m. | 3 | 0 % |
| hole | 3 | 0 % |
| singularity | 3 | 0 % |
| compressibility | 3 | 0 % |
| 6 | 3 | 0 % |
| stoffel | 3 | 0 % |
| files | 3 | 0 % |
| g | 3 | 0 % |
| damping | 3 | 0 % |
| dynamic | 3 | 0 % |
| logvinovich | 3 | 0 % |
| integral | 3 | 0 % |
| radial | 3 | 0 % |
| correction | 3 | 0 % |
| natural | 3 | 0 % |
| bubbly | 3 | 0 % |
| govindarajan | 3 | 0 % |
| gowing | 3 | 0 % |
| partial | 3 | 0 % |
| instabilities | 3 | 0 % |
| bearings | 3 | 0 % |
| phenomena | 3 | 0 % |
| micro | 3 | 0 % |
| andreas | 3 | 0 % |
| experience | 3 | 0 % |
| machinery | 3 | 0 % |
| session | 3 | 0 % |
| level | 3 | 0 % |
| franc | 3 | 0 % |
| circular | 3 | 0 % |
| homogeneous | 3 | 0 % |
| 66 | 3 | 0 % |
| 1998 | 3 | 0 % |
| kuklinski | 3 | 0 % |
| vorticity | 3 | 0 % |
| henoch | 3 | 0 % |
| 3 | 3 | 0 % |
| modle | 2 | 0 % |
| projectile | 2 | 0 % |
| load | 2 | 0 % |
| particle | 2 | 0 % |
| calculations | 2 | 0 % |
| basin | 2 | 0 % |
| gravity | 2 | 0 % |
| scaling | 2 | 0 % |
| rule | 2 | 0 % |
| maccormack | 2 | 0 % |
| shockwave | 2 | 0 % |
| reduce | 2 | 0 % |
| ganippa | 2 | 0 % |
| nonspherical | 2 | 0 % |
| can | 2 | 0 % |
| henrik | 2 | 0 % |
| curves | 2 | 0 % |
| fluent-pdf | 2 | 0 % |
| -sridhar | 2 | 0 % |
| lab | 2 | 0 % |
| t. | 2 | 0 % |
| hardness | 2 | 0 % |
| nasa | 2 | 0 % |
| microbubble | 2 | 0 % |
| vertical | 2 | 0 % |
| astolfi | 2 | 0 % |
| project | 2 | 0 % |
| ukon | 2 | 0 % |
| mechanics | 2 | 0 % |
| proceedings | 2 | 0 % |
| agressiveness | 2 | 0 % |
| mech. | 2 | 0 % |
| produced | 2 | 0 % |
| software | 2 | 0 % |
| cavitationpar | 2 | 0 % |
| inlet | 2 | 0 % |
| fast | 2 | 0 % |
| maneauver | 2 | 0 % |
| rate | 2 | 0 % |
| inner | 2 | 0 % |
| presented | 2 | 0 % |
| gopalan | 2 | 0 % |
| weber | 2 | 0 % |
| hopkins | 2 | 0 % |
| partially | 2 | 0 % |
| kavitation | 2 | 0 % |
| lift | 2 | 0 % |
| submergence | 2 | 0 % |
| california | 2 | 0 % |
| shf | 2 | 0 % |
| reactor | 2 | 0 % |
| sydney | 2 | 0 % |
| 3% | 2 | 0 % |
| initially | 2 | 0 % |
| axis | 2 | 0 % |
| fluctuations | 2 | 0 % |
| express | 2 | 0 % |
| 1 | 2 | 0 % |
| stress | 2 | 0 % |
| models | 2 | 0 % |
| swept | 2 | 0 % |
| skew | 2 | 0 % |
| de | 2 | 0 % |
| considerations | 2 | 0 % |
| relation | 2 | 0 % |
| liquids | 2 | 0 % |
| multiperforated | 2 | 0 % |
| kanplan | 2 | 0 % |
| machine | 2 | 0 % |
| boundry | 2 | 0 % |
| plane | 2 | 0 % |
| he | 2 | 0 % |
| radius | 2 | 0 % |
| changing | 2 | 0 % |
| photo | 2 | 0 % |
| pit | 2 | 0 % |
| booster | 2 | 0 % |
| lohrberg | 2 | 0 % |
| 200 | 2 | 0 % |
| Ⅱ | 2 | 0 % |
| \xec\xa0\x80\xec\x9e\x90 | 2 | 0 % |
| g.v. | 2 | 0 % |
| sump | 2 | 0 % |
| final | 2 | 0 % |
| introduction | 2 | 0 % |
| mccormick | 2 | 0 % |
| savchenko | 2 | 0 % |
| spectral | 2 | 0 % |
| dimensional | 2 | 0 % |
| meters | 2 | 0 % |
| patella | 2 | 0 % |
| schematic | 2 | 0 % |
| pipes | 2 | 0 % |
| fluids | 2 | 0 % |
| alajbegovic | 2 | 0 % |
| hydrodynamics | 2 | 0 % |
| sonic | 2 | 0 % |
| akamatsu | 2 | 0 % |
| plankton | 2 | 0 % |
| uniform | 2 | 0 % |
| axial-flow | 2 | 0 % |
| webkr | 2 | 0 % |
| valves | 2 | 0 % |
| template | 2 | 0 % |
| fluent5 | 2 | 0 % |
| ” | 2 | 0 % |
| overview | 2 | 0 % |
| tension | 2 | 0 % |
| optimization | 2 | 0 % |
| torpedo | 2 | 0 % |
| hakimi | 2 | 0 % |
| under | 2 | 0 % |
| jessup | 2 | 0 % |
| m | 2 | 0 % |
| oil | 2 | 0 % |
| fluctuation | 2 | 0 % |
| impulsive | 2 | 0 % |
| db | 2 | 0 % |
| missiles | 2 | 0 % |
| naca16 | 2 | 0 % |
| measurements | 2 | 0 % |
| coutier | 2 | 0 % |
| propulsion | 2 | 0 % |
| transfer | 2 | 0 % |
| multiorifice | 2 | 0 % |
| real | 2 | 0 % |
| radiated | 2 | 0 % |
| large | 2 | 0 % |
| lithotripsy | 2 | 0 % |
| nominal | 2 | 0 % |
| non | 2 | 0 % |
| hydro | 2 | 0 % |
| atlar | 2 | 0 % |
| expression | 2 | 0 % |
| brennen | 2 | 0 % |
| process | 2 | 0 % |
| treatment | 2 | 0 % |
| kinnas | 2 | 0 % |
| strain | 2 | 0 % |
| interaction | 2 | 0 % |
| 作者 | 2 | 0 % |
| x | 2 | 0 % |
| sant | 2 | 0 % |
| center | 2 | 0 % |
| non-cavitating | 2 | 0 % |
| intakes | 2 | 0 % |
| breakdown | 2 | 0 % |
| force | 2 | 0 % |
| podded | 2 | 0 % |
| book | 2 | 0 % |
| vs | 2 | 0 % |
| saturation | 2 | 0 % |
| pvdf | 2 | 0 % |
| code | 2 | 0 % |
| discuss | 2 | 0 % |
| history | 2 | 0 % |
| re-entrant | 2 | 0 % |
| modeles | 2 | 0 % |
| raabe | 2 | 0 % |
| sumps | 2 | 0 % |
| nakatake | 2 | 0 % |
| image | 2 | 0 % |
| turbopumps | 2 | 0 % |
| photography | 2 | 0 % |
| mixture | 2 | 0 % |
| dx | 2 | 0 % |
| kalumuck | 2 | 0 % |
| profiles | 2 | 0 % |
| lagrangian | 2 | 0 % |
| hollow | 2 | 0 % |
| senocak | 2 | 0 % |
| j-castano | 2 | 0 % |
| mechanisms | 2 | 0 % |
| erosive | 2 | 0 % |
| bem | 2 | 0 % |
| cp | 2 | 0 % |
| porous | 2 | 0 % |
| electrolysis | 2 | 0 % |
| 37 | 2 | 0 % |
| why | 2 | 0 % |
| backflow | 2 | 0 % |
| vehicles.pdf | 2 | 0 % |
| day | 2 | 0 % |
| hub | 2 | 0 % |
| turbin | 2 | 0 % |
| difference | 2 | 0 % |
| laser-induced | 2 | 0 % |
| proceedings- | 2 | 0 % |
| specific | 2 | 0 % |
| defferents | 2 | 0 % |
| cryogenic | 2 | 0 % |
| japikse | 2 | 0 % |
| int. | 2 | 0 % |
| setup | 2 | 0 % |
| ariane | 2 | 0 % |
| solving | 2 | 0 % |
| dimension | 2 | 0 % |
| neighborhood | 2 | 0 % |
| centre | 2 | 0 % |
| strategies | 2 | 0 % |
| et | 2 | 0 % |
| prevention | 2 | 0 % |
| chimera | 2 | 0 % |
| throat | 2 | 0 % |
| cavitaion | 2 | 0 % |
| downstream | 2 | 0 % |
| three | 2 | 0 % |
| simulations | 2 | 0 % |
| stuart | 2 | 0 % |
| h. | 2 | 0 % |
| tests | 2 | 0 % |
| results | 2 | 0 % |
| enhance | 2 | 0 % |
| conclusion | 2 | 0 % |
| ser. | 2 | 0 % |
| increment | 2 | 0 % |
| viscous | 2 | 0 % |
| inverse | 2 | 0 % |
| “numerical | 2 | 0 % |
| machines | 2 | 0 % |
| tube | 2 | 0 % |
| magnitude | 2 | 0 % |
| area | 2 | 0 % |
| forces | 2 | 0 % |
| w. | 2 | 0 % |
| root-cavitation | 2 | 0 % |
| weitendorf | 2 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 2 | 0 % |
| navier | 2 | 0 % |
| fields | 2 | 0 % |
| crash | 2 | 0 % |
| profile | 2 | 0 % |
| tplox | 2 | 0 % |
| thrust | 2 | 0 % |
| a. | 2 | 0 % |
| rms | 2 | 0 % |
| submarine | 2 | 0 % |
| computation | 2 | 0 % |
| heater | 2 | 0 % |
| momentum | 2 | 0 % |
| fission | 2 | 0 % |
| freshwater | 2 | 0 % |
| lauterborn | 2 | 0 % |
| andreasin | 2 | 0 % |
| ph. | 2 | 0 % |
| limit | 2 | 0 % |
| holes | 2 | 0 % |
| fujikawa | 2 | 0 % |
| penn | 2 | 0 % |
| validation | 2 | 0 % |
| lattice | 2 | 0 % |
| phd | 2 | 0 % |
| one | 2 | 0 % |
| v. | 2 | 0 % |
| grekula | 2 | 0 % |
| inc | 2 | 0 % |
| drop | 2 | 0 % |
| schiebe | 2 | 0 % |
| installation | 2 | 0 % |
| find | 2 | 0 % |
| hydroacoustic | 2 | 0 % |
| cruiser | 2 | 0 % |
| turbo-machinery | 2 | 0 % |
| material | 2 | 0 % |
| lifting | 2 | 0 % |
| main | 2 | 0 % |
| near | 2 | 0 % |
| hammer | 2 | 0 % |
| dumont | 2 | 0 % |
| preconditioning | 2 | 0 % |
| photos | 2 | 0 % |
| vehicles | 2 | 0 % |
| pumps.pdf | 2 | 0 % |
| passenger | 2 | 0 % |
| cavity-running | 2 | 0 % |
| 3-d | 2 | 0 % |
| picture | 2 | 0 % |
| absorbed | 2 | 0 % |
| al. | 2 | 0 % |
| particles | 2 | 0 % |
| hydroacoustics | 2 | 0 % |
| leakage | 2 | 0 % |
| cavitation-journal | 2 | 0 % |
| slender | 2 | 0 % |
| mpa | 1 | 0 % |
| murtuza | 1 | 0 % |
| centrifgal | 1 | 0 % |
| n. | 1 | 0 % |
| cavitations.pdf | 1 | 0 % |
| serebryakov | 1 | 0 % |
| reasons | 1 | 0 % |
| materials | 1 | 0 % |
| go.jp | 1 | 0 % |
| bellows | 1 | 0 % |
| restrictor | 1 | 0 % |
| cylinder | 1 | 0 % |
| yuriy | 1 | 0 % |
| vessels | 1 | 0 % |
| explained | 1 | 0 % |
| figures | 1 | 0 % |
| where | 1 | 0 % |
| average | 1 | 0 % |
| blade-sheet | 1 | 0 % |
| kulkinski | 1 | 0 % |
| carolyn | 1 | 0 % |
| coefficients | 1 | 0 % |
| linear-vortex-source | 1 | 0 % |
| subsonic | 1 | 0 % |
| bolle | 1 | 0 % |
| lomax | 1 | 0 % |
| circular-cylindrical | 1 | 0 % |
| cause | 1 | 0 % |
| arc | 1 | 0 % |
| navier-stokes | 1 | 0 % |
| 1954 | 1 | 0 % |
| astern | 1 | 0 % |
| 16-012 | 1 | 0 % |
| hydropower | 1 | 0 % |
| shin | 1 | 0 % |
| inch | 1 | 0 % |
| 2-d | 1 | 0 % |
| sewage | 1 | 0 % |
| venkateswaran | 1 | 0 % |
| interesting | 1 | 0 % |
| sweep | 1 | 0 % |
| -non-spherical | 1 | 0 % |
| problem | 1 | 0 % |
| spheroidal | 1 | 0 % |
| comparaison | 1 | 0 % |
| coalescence | 1 | 0 % |
| mohamed | 1 | 0 % |
| requirements | 1 | 0 % |
| 8 | 1 | 0 % |
| medwins | 1 | 0 % |
| laminar | 1 | 0 % |
| propulsor | 1 | 0 % |
| pinkus | 1 | 0 % |
| taib | 1 | 0 % |
| cavity-flow | 1 | 0 % |
| gurevich | 1 | 0 % |
| tables | 1 | 0 % |
| strip | 1 | 0 % |
| explosion | 1 | 0 % |
| bergwerk | 1 | 0 % |
| miniature | 1 | 0 % |
| nonlifting | 1 | 0 % |
| henda | 1 | 0 % |
| top | 1 | 0 % |
| pump/pdf | 1 | 0 % |
| stress- | 1 | 0 % |
| conditions | 1 | 0 % |
| protection | 1 | 0 % |
| source | 1 | 0 % |
| computing | 1 | 0 % |
| measuring | 1 | 0 % |
| local | 1 | 0 % |
| 107 | 1 | 0 % |
| skeg | 1 | 0 % |
| documentation | 1 | 0 % |
| judge | 1 | 0 % |
| akinori | 1 | 0 % |
| esposito | 1 | 0 % |
| tangential | 1 | 0 % |
| rd | 1 | 0 % |
| max | 1 | 0 % |
| 0012 | 1 | 0 % |
| szeri | 1 | 0 % |
| pitch | 1 | 0 % |
| rayleigh-plesset | 1 | 0 % |
| ring | 1 | 0 % |
| bell | 1 | 0 % |
| reverse | 1 | 0 % |
| conclution | 1 | 0 % |
| blowing | 1 | 0 % |
| price | 1 | 0 % |
| flat | 1 | 0 % |
| allmaras | 1 | 0 % |
| burril | 1 | 0 % |
| 1975 | 1 | 0 % |
| ac.uk | 1 | 0 % |
| yoshizawa | 1 | 0 % |
| boiling | 1 | 0 % |
| 1973 | 1 | 0 % |
| gary | 1 | 0 % |
| mehmet | 1 | 0 % |
| naca0020 | 1 | 0 % |
| oscillation | 1 | 0 % |
| duffing | 1 | 0 % |
| predictor-corrector | 1 | 0 % |
| duke | 1 | 0 % |
| gabrielli | 1 | 0 % |
| evaluationof | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| georges | 1 | 0 % |
| loads | 1 | 0 % |
| dimensions | 1 | 0 % |
| swath | 1 | 0 % |
| -springerlink | 1 | 0 % |
| thermal | 1 | 0 % |
| dtmb | 1 | 0 % |
| explicit | 1 | 0 % |
| 1993 | 1 | 0 % |
| probellers | 1 | 0 % |
| flat-element | 1 | 0 % |
| 1983 | 1 | 0 % |
| fixed | 1 | 0 % |
| meyne | 1 | 0 % |
| numericals | 1 | 0 % |
| gas-particle | 1 | 0 % |
| newcastle | 1 | 0 % |
| treatments | 1 | 0 % |
| pei | 1 | 0 % |
| eroding | 1 | 0 % |
| g. | 1 | 0 % |
| lecture | 1 | 0 % |
| cambridge | 1 | 0 % |
| exchange | 1 | 0 % |
| two-phase | 1 | 0 % |
| precondition | 1 | 0 % |
| similar | 1 | 0 % |
| fujii | 1 | 0 % |
| ellipse | 1 | 0 % |
| curvilinear | 1 | 0 % |
| takahara | 1 | 0 % |
| a9 | 1 | 0 % |
| finding | 1 | 0 % |
| goirand | 1 | 0 % |
| rapposelli | 1 | 0 % |
| devices | 1 | 0 % |
| emilio | 1 | 0 % |
| building | 1 | 0 % |
| unstable | 1 | 0 % |
| dr. | 1 | 0 % |
| drain | 1 | 0 % |
| arl | 1 | 0 % |
| specification | 1 | 0 % |
| merging | 1 | 0 % |
| make | 1 | 0 % |
| explanation | 1 | 0 % |
| evolution | 1 | 0 % |
| djeridi | 1 | 0 % |
| passing | 1 | 0 % |
| seawater | 1 | 0 % |
| table | 1 | 0 % |
| immersion | 1 | 0 % |
| undersea | 1 | 0 % |
| line | 1 | 0 % |
| utilization | 1 | 0 % |
| similarity | 1 | 0 % |
| atomization | 1 | 0 % |
| saito | 1 | 0 % |
| secondary | 1 | 0 % |
| result | 1 | 0 % |
| recirculation | 1 | 0 % |
| orders | 1 | 0 % |
| function | 1 | 0 % |
| streamline | 1 | 0 % |
| skeg-rudders | 1 | 0 % |
| codes | 1 | 0 % |
| auton | 1 | 0 % |
| haberman | 1 | 0 % |
| lcc | 1 | 0 % |
| reflection | 1 | 0 % |
| rans | 1 | 0 % |
| reflecting | 1 | 0 % |
| film | 1 | 0 % |
| aspects | 1 | 0 % |
| set | 1 | 0 % |
| horns | 1 | 0 % |
| auf | 1 | 0 % |
| burger | 1 | 0 % |
| tragectory | 1 | 0 % |
| spot | 1 | 0 % |
| lokhandwalla | 1 | 0 % |
| gov | 1 | 0 % |
| ahead | 1 | 0 % |
| berntsen | 1 | 0 % |
| agent | 1 | 0 % |
| counting | 1 | 0 % |
| e.-a. | 1 | 0 % |
| investigations | 1 | 0 % |
| sakoda | 1 | 0 % |
| location | 1 | 0 % |
| velocimetry | 1 | 0 % |
| 250 | 1 | 0 % |
| ioannides | 1 | 0 % |
| waterjets | 1 | 0 % |
| gov.uk | 1 | 0 % |
| lectures | 1 | 0 % |
| reynolds | 1 | 0 % |
| furukawa | 1 | 0 % |
| young | 1 | 0 % |
| solutions | 1 | 0 % |
| trials | 1 | 0 % |
| laser-inducedbubbles | 1 | 0 % |
| working | 1 | 0 % |
| aspect | 1 | 0 % |
| space | 1 | 0 % |
| restrictive | 1 | 0 % |
| heating | 1 | 0 % |
| kinds | 1 | 0 % |
| cormick | 1 | 0 % |
| vortexing | 1 | 0 % |
| tim | 1 | 0 % |
| parallel | 1 | 0 % |
| conical | 1 | 0 % |
| 006 | 1 | 0 % |
| clark-y | 1 | 0 % |
| npsh | 1 | 0 % |
| lengths | 1 | 0 % |
| vector | 1 | 0 % |
| tutorials | 1 | 0 % |
| period | 1 | 0 % |
| pump.pdf | 1 | 0 % |
| y. | 1 | 0 % |
| witnessed | 1 | 0 % |
| presents | 1 | 0 % |
| free-stream | 1 | 0 % |
| attack | 1 | 0 % |
| buffer | 1 | 0 % |
| all | 1 | 0 % |
| sigma | 1 | 0 % |
| velocities | 1 | 0 % |
| levels | 1 | 0 % |
| supercavitation.pdf | 1 | 0 % |
| plants | 1 | 0 % |
| co. | 1 | 0 % |
| works- | 1 | 0 % |
| trial | 1 | 0 % |
| remove | 1 | 0 % |
| friesch | 1 | 0 % |
| france | 1 | 0 % |
| kill | 1 | 0 % |
| yfglk | 1 | 0 % |
| preston | 1 | 0 % |
| runge-kutta | 1 | 0 % |
| salt | 1 | 0 % |
| scattering | 1 | 0 % |
| relate | 1 | 0 % |
| colonius | 1 | 0 % |
| symposia | 1 | 0 % |
| munitions | 1 | 0 % |
| impellers | 1 | 0 % |
| siam | 1 | 0 % |
| shedding | 1 | 0 % |
| naca0009 | 1 | 0 % |
| two-body | 1 | 0 % |
| ashwin | 1 | 0 % |
| pattern | 1 | 0 % |
| hiroyasu | 1 | 0 % |
| figers | 1 | 0 % |
| destruction | 1 | 0 % |
| Γ | 1 | 0 % |
| pits | 1 | 0 % |
| tensile | 1 | 0 % |
| voltex | 1 | 0 % |
| fingers | 1 | 0 % |
| behaviour | 1 | 0 % |
| black | 1 | 0 % |
| addedmass | 1 | 0 % |
| foam | 1 | 0 % |
| lichtarowicz | 1 | 0 % |
| ln2 | 1 | 0 % |
| hosangadi | 1 | 0 % |
| ristriction | 1 | 0 % |
| physics | 1 | 0 % |
| osaka | 1 | 0 % |
| create | 1 | 0 % |
| proc. | 1 | 0 % |
| edges | 1 | 0 % |
| bolla | 1 | 0 % |
| single | 1 | 0 % |
| signal | 1 | 0 % |
| observe | 1 | 0 % |
| shaped | 1 | 0 % |
| mod | 1 | 0 % |
| hot | 1 | 0 % |
| self | 1 | 0 % |
| pitcures | 1 | 0 % |
| chahine | 1 | 0 % |
| gap | 1 | 0 % |
| t | 1 | 0 % |
| matsumoto | 1 | 0 % |
| deaerated | 1 | 0 % |
| stresses | 1 | 0 % |
| condensable | 1 | 0 % |
| Other words | 507 | 7.8 % |
|