| 1194 different keywords | Search | Percent |
|---|
| cavitation | 356 | 7.9 % |
| of | 133 | 2.9 % |
| pdf | 126 | 2.8 % |
| pump | 96 | 2.1 % |
| propeller | 78 | 1.7 % |
| in | 54 | 1.2 % |
| on | 53 | 1.1 % |
| flow | 51 | 1.1 % |
| orifice | 48 | 1 % |
| vortex | 47 | 1 % |
| bubble | 45 | 1 % |
| and | 45 | 1 % |
| centrifugal | 45 | 1 % |
| the | 44 | 0.9 % |
| fluent | 42 | 0.9 % |
| supercavitation | 39 | 0.8 % |
| restriction | 37 | 0.8 % |
| filetype | 35 | 0.7 % |
| inducer | 34 | 0.7 % |
| for | 34 | 0.7 % |
| design | 27 | 0.6 % |
| tip | 25 | 0.5 % |
| pressure | 24 | 0.5 % |
| analysis | 24 | 0.5 % |
| water | 24 | 0.5 % |
| kaplan | 24 | 0.5 % |
| turbine | 23 | 0.5 % |
| a | 22 | 0.4 % |
| erosion | 21 | 0.4 % |
| cavitating | 20 | 0.4 % |
| numerical | 19 | 0.4 % |
| symposium | 19 | 0.4 % |
| international | 19 | 0.4 % |
| effect | 19 | 0.4 % |
| calculation | 19 | 0.4 % |
| blade | 18 | 0.4 % |
| tunnel | 18 | 0.4 % |
| pumps | 18 | 0.4 % |
| surface | 17 | 0.3 % |
| hydrodynamic | 17 | 0.3 % |
| model | 16 | 0.3 % |
| modeling | 16 | 0.3 % |
| equation | 16 | 0.3 % |
| cfd | 16 | 0.3 % |
| rudder | 16 | 0.3 % |
| bubbles | 15 | 0.3 % |
| hydrofoil | 15 | 0.3 % |
| supercavitating | 15 | 0.3 % |
| types | 15 | 0.3 % |
| suction | 15 | 0.3 % |
| jet | 14 | 0.3 % |
| orifices | 14 | 0.3 % |
| joint | 14 | 0.3 % |
| number | 13 | 0.2 % |
| to | 13 | 0.2 % |
| cav2001 | 13 | 0.2 % |
| method | 13 | 0.2 % |
| nexearch | 13 | 0.2 % |
| speed | 12 | 0.2 % |
| ship | 12 | 0.2 % |
| dynamics | 11 | 0.2 % |
| damage | 11 | 0.2 % |
| propellers | 11 | 0.2 % |
| frequency | 11 | 0.2 % |
| horn | 10 | 0.2 % |
| azipod | 10 | 0.2 % |
| study | 10 | 0.2 % |
| unsteady | 10 | 0.2 % |
| naca | 10 | 0.2 % |
| nozzle | 10 | 0.2 % |
| effects | 10 | 0.2 % |
| liquid | 9 | 0.2 % |
| 2001 | 9 | 0.2 % |
| coefficient | 9 | 0.2 % |
| time-frequency | 9 | 0.2 % |
| boundary | 9 | 0.2 % |
| thesis | 9 | 0.2 % |
| plate | 9 | 0.2 % |
| simulation | 9 | 0.2 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 9 | 0.2 % |
| two | 9 | 0.2 % |
| gas | 9 | 0.2 % |
| ships | 9 | 0.2 % |
| rayleigh | 9 | 0.2 % |
| at | 9 | 0.2 % |
| piercing | 9 | 0.2 % |
| turbopump | 8 | 0.1 % |
| mass | 8 | 0.1 % |
| how | 8 | 0.1 % |
| scale | 8 | 0.1 % |
| bodies | 8 | 0.1 % |
| hull | 8 | 0.1 % |
| distribution | 8 | 0.1 % |
| flows | 8 | 0.1 % |
| rocket | 8 | 0.1 % |
| time | 8 | 0.1 % |
| impeller | 8 | 0.1 % |
| cavity | 8 | 0.1 % |
| cav | 8 | 0.1 % |
| high | 8 | 0.1 % |
| noise | 8 | 0.1 % |
| measurement | 7 | 0.1 % |
| experiment | 7 | 0.1 % |
| fluid | 7 | 0.1 % |
| by | 7 | 0.1 % |
| collapse | 7 | 0.1 % |
| sump | 7 | 0.1 % |
| panel | 7 | 0.1 % |
| cavitator | 7 | 0.1 % |
| added | 7 | 0.1 % |
| using | 7 | 0.1 % |
| methods | 7 | 0.1 % |
| blades | 7 | 0.1 % |
| weitendorf | 7 | 0.1 % |
| sheet | 7 | 0.1 % |
| hydraulic | 7 | 0.1 % |
| inception | 7 | 0.1 % |
| experimental | 7 | 0.1 % |
| what | 6 | 0.1 % |
| phase | 6 | 0.1 % |
| trailing | 6 | 0.1 % |
| vortices | 6 | 0.1 % |
| drag | 6 | 0.1 % |
| video | 6 | 0.1 % |
| test | 6 | 0.1 % |
| oscillation | 6 | 0.1 % |
| [pdf] | 6 | 0.1 % |
| aisi | 6 | 0.1 % |
| free | 6 | 0.1 % |
| foil | 6 | 0.1 % |
| sae | 6 | 0.1 % |
| wake | 6 | 0.1 % |
| hydro | 6 | 0.1 % |
| vibration | 6 | 0.1 % |
| wave | 6 | 0.1 % |
| shock | 6 | 0.1 % |
| chahine | 6 | 0.1 % |
| airfoil | 6 | 0.1 % |
| plesset | 6 | 0.1 % |
| laboratory | 6 | 0.1 % |
| photos | 6 | 0.1 % |
| projectile | 5 | 0.1 % |
| underwater | 5 | 0.1 % |
| vertical | 5 | 0.1 % |
| type | 5 | 0.1 % |
| inlet | 5 | 0.1 % |
| ea | 5 | 0.1 % |
| journal | 5 | 0.1 % |
| intake | 5 | 0.1 % |
| supersonic | 5 | 0.1 % |
| performance | 5 | 0.1 % |
| formed | 5 | 0.1 % |
| & | 5 | 0.1 % |
| formula | 5 | 0.1 % |
| sound | 5 | 0.1 % |
| vibrations | 5 | 0.1 % |
| savchenko | 5 | 0.1 % |
| paper | 5 | 0.1 % |
| stokes | 5 | 0.1 % |
| with | 5 | 0.1 % |
| velocity | 5 | 0.1 % |
| angle | 5 | 0.1 % |
| atlar | 5 | 0.1 % |
| application | 5 | 0.1 % |
| injection | 5 | 0.1 % |
| turbin | 5 | 0.1 % |
| size | 5 | 0.1 % |
| steel | 5 | 0.1 % |
| diesel | 5 | 0.1 % |
| damping | 5 | 0.1 % |
| forces | 5 | 0.1 % |
| scott | 5 | 0.1 % |
| investigation | 5 | 0.1 % |
| helium | 5 | 0.1 % |
| gowing | 5 | 0.1 % |
| supercavity | 5 | 0.1 % |
| structure | 5 | 0.1 % |
| shapes | 4 | 0 % |
| energy | 4 | 0 % |
| helical | 4 | 0 % |
| ihm | 4 | 0 % |
| equations | 4 | 0 % |
| pipe | 4 | 0 % |
| nuclei | 4 | 0 % |
| axial | 4 | 0 % |
| de | 4 | 0 % |
| azimuthal | 4 | 0 % |
| introduction | 4 | 0 % |
| is | 4 | 0 % |
| quality | 4 | 0 % |
| propellor | 4 | 0 % |
| asme | 4 | 0 % |
| turbines | 4 | 0 % |
| loading | 4 | 0 % |
| inducers | 4 | 0 % |
| sizing | 4 | 0 % |
| arakeri | 4 | 0 % |
| capture | 4 | 0 % |
| theory | 4 | 0 % |
| compressible | 4 | 0 % |
| are | 4 | 0 % |
| pictures | 4 | 0 % |
| npsh | 4 | 0 % |
| reduction | 4 | 0 % |
| technology | 4 | 0 % |
| 0015 | 4 | 0 % |
| ukraine | 4 | 0 % |
| wigner | 4 | 0 % |
| problems | 4 | 0 % |
| hosangadi | 4 | 0 % |
| body | 4 | 0 % |
| characteristics | 4 | 0 % |
| during | 4 | 0 % |
| japikse | 4 | 0 % |
| cloud | 4 | 0 % |
| volume | 4 | 0 % |
| .edu | 4 | 0 % |
| turbo | 4 | 0 % |
| dam | 4 | 0 % |
| phenomena | 4 | 0 % |
| alternate | 4 | 0 % |
| aircraft | 4 | 0 % |
| site | 4 | 0 % |
| 1055 | 4 | 0 % |
| kamiirisa | 4 | 0 % |
| air | 4 | 0 % |
| particle | 3 | 0 % |
| calculations | 3 | 0 % |
| thermodynamic | 3 | 0 % |
| author | 3 | 0 % |
| fraction | 3 | 0 % |
| super | 3 | 0 % |
| polytropic | 3 | 0 % |
| subsonic | 3 | 0 % |
| hydrogen | 3 | 0 % |
| different | 3 | 0 % |
| fatigue | 3 | 0 % |
| 1015 | 3 | 0 % |
| heat | 3 | 0 % |
| injector | 3 | 0 % |
| institute | 3 | 0 % |
| laser | 3 | 0 % |
| about | 3 | 0 % |
| algorithm | 3 | 0 % |
| oscillations | 3 | 0 % |
| flat | 3 | 0 % |
| vof | 3 | 0 % |
| eulerian | 3 | 0 % |
| grenoble | 3 | 0 % |
| cone | 3 | 0 % |
| butterfly | 3 | 0 % |
| law | 3 | 0 % |
| two-phase | 3 | 0 % |
| rotating | 3 | 0 % |
| based | 3 | 0 % |
| surge | 3 | 0 % |
| developed | 3 | 0 % |
| solution | 3 | 0 % |
| david | 3 | 0 % |
| v | 3 | 0 % |
| engine | 3 | 0 % |
| turbomachinery | 3 | 0 % |
| reynolds | 3 | 0 % |
| shape | 3 | 0 % |
| intakes | 3 | 0 % |
| naca0012 | 3 | 0 % |
| l | 3 | 0 % |
| strouhal | 3 | 0 % |
| influenced | 3 | 0 % |
| two-dimensional | 3 | 0 % |
| data | 3 | 0 % |
| mechanism | 3 | 0 % |
| spherical | 3 | 0 % |
| cd | 3 | 0 % |
| hiroyasu | 3 | 0 % |
| 5 | 3 | 0 % |
| ultrasound | 3 | 0 % |
| discharge | 3 | 0 % |
| blade. | 3 | 0 % |
| hub | 3 | 0 % |
| foam | 3 | 0 % |
| tanguay | 3 | 0 % |
| contours | 3 | 0 % |
| stabilization | 3 | 0 % |
| 1996 | 3 | 0 % |
| transient | 3 | 0 % |
| simulations | 3 | 0 % |
| h. | 3 | 0 % |
| prediction | 3 | 0 % |
| void | 3 | 0 % |
| thruster | 3 | 0 % |
| thrust | 3 | 0 % |
| bubbly | 3 | 0 % |
| computation | 3 | 0 % |
| criteria | 3 | 0 % |
| curve | 3 | 0 % |
| full | 3 | 0 % |
| instabilities | 3 | 0 % |
| rarefaction | 3 | 0 % |
| condition | 3 | 0 % |
| cavitations | 3 | 0 % |
| franc | 3 | 0 % |
| 66 | 3 | 0 % |
| ashvin | 3 | 0 % |
| michel | 3 | 0 % |
| calculate | 3 | 0 % |
| near | 3 | 0 % |
| picture | 3 | 0 % |
| mach | 2 | 0 % |
| caviation | 2 | 0 % |
| martin | 2 | 0 % |
| basin | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| sessionb3.003 | 2 | 0 % |
| electromagnetic | 2 | 0 % |
| 4th | 2 | 0 % |
| marine | 2 | 0 % |
| schaffar | 2 | 0 % |
| figures | 2 | 0 % |
| static | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| exp | 2 | 0 % |
| setting | 2 | 0 % |
| 2-d | 2 | 0 % |
| runner | 2 | 0 % |
| moutant | 2 | 0 % |
| sclavounos | 2 | 0 % |
| industrial | 2 | 0 % |
| incompressible | 2 | 0 % |
| stutz | 2 | 0 % |
| caltech | 2 | 0 % |
| grid | 2 | 0 % |
| tamura | 2 | 0 % |
| .prediction | 2 | 0 % |
| kyowa | 2 | 0 % |
| numerically | 2 | 0 % |
| perspectives | 2 | 0 % |
| vapor | 2 | 0 % |
| explosion | 2 | 0 % |
| lift | 2 | 0 % |
| case | 2 | 0 % |
| influence | 2 | 0 % |
| blunt | 2 | 0 % |
| counter-jet | 2 | 0 % |
| instability | 2 | 0 % |
| state | 2 | 0 % |
| fluctuations | 2 | 0 % |
| crack | 2 | 0 % |
| models | 2 | 0 % |
| rayleigh-plesset | 2 | 0 % |
| propulsors | 2 | 0 % |
| taylor | 2 | 0 % |
| ring | 2 | 0 % |
| skew | 2 | 0 % |
| r. | 2 | 0 % |
| hydraulics | 2 | 0 % |
| liquids | 2 | 0 % |
| chart | 2 | 0 % |
| rules | 2 | 0 % |
| oxygen | 2 | 0 % |
| 213 | 2 | 0 % |
| naca0020 | 2 | 0 % |
| design. | 2 | 0 % |
| reentrant | 2 | 0 % |
| thermal | 2 | 0 % |
| naca66 | 2 | 0 % |
| ch4 | 2 | 0 % |
| explicit | 2 | 0 % |
| 468 | 2 | 0 % |
| intitle | 2 | 0 % |
| fluids | 2 | 0 % |
| prevent | 2 | 0 % |
| sonic | 2 | 0 % |
| cremhyg | 2 | 0 % |
| were | 2 | 0 % |
| tvip2000 | 2 | 0 % |
| acoustic | 2 | 0 % |
| unstable | 2 | 0 % |
| low | 2 | 0 % |
| takemura | 2 | 0 % |
| maitre | 2 | 0 % |
| layout | 2 | 0 % |
| impacts | 2 | 0 % |
| layer | 2 | 0 % |
| b | 2 | 0 % |
| ventilated | 2 | 0 % |
| channel | 2 | 0 % |
| motion | 2 | 0 % |
| shocks | 2 | 0 % |
| trajectory | 2 | 0 % |
| camera | 2 | 0 % |
| stripling | 2 | 0 % |
| stft | 2 | 0 % |
| field | 2 | 0 % |
| sturtevant | 2 | 0 % |
| s. | 2 | 0 % |
| propeler | 2 | 0 % |
| p.h.d. | 2 | 0 % |
| interaction | 2 | 0 % |
| fortes-patella | 2 | 0 % |
| edge | 2 | 0 % |
| reboud | 2 | 0 % |
| videos | 2 | 0 % |
| halsted | 2 | 0 % |
| vs | 2 | 0 % |
| 3d | 2 | 0 % |
| thierry | 2 | 0 % |
| code | 2 | 0 % |
| turbulent | 2 | 0 % |
| comparison | 2 | 0 % |
| microscope | 2 | 0 % |
| nozzles | 2 | 0 % |
| - | 2 | 0 % |
| sketches | 2 | 0 % |
| turbopumps | 2 | 0 % |
| 1948 | 2 | 0 % |
| bellmouth | 2 | 0 % |
| imacon | 2 | 0 % |
| lagrangian | 2 | 0 % |
| total | 2 | 0 % |
| coupling | 2 | 0 % |
| fruman | 2 | 0 % |
| gust | 2 | 0 % |
| roughness | 2 | 0 % |
| shedding | 2 | 0 % |
| factor | 2 | 0 % |
| mechanisms | 2 | 0 % |
| control | 2 | 0 % |
| vehickes | 2 | 0 % |
| spillway | 2 | 0 % |
| angles | 2 | 0 % |
| shear | 2 | 0 % |
| d | 2 | 0 % |
| maneuvering | 2 | 0 % |
| applications | 2 | 0 % |
| scheme | 2 | 0 % |
| swirl | 2 | 0 % |
| spray | 2 | 0 % |
| cryogenic | 2 | 0 % |
| single | 2 | 0 % |
| mod | 2 | 0 % |
| critical | 2 | 0 % |
| gap | 2 | 0 % |
| solving | 2 | 0 % |
| evaluation | 2 | 0 % |
| compressibility | 2 | 0 % |
| chimera | 2 | 0 % |
| semenenko | 2 | 0 % |
| o. | 2 | 0 % |
| cavitaion | 2 | 0 % |
| downstream | 2 | 0 % |
| s55c | 2 | 0 % |
| collapsing | 2 | 0 % |
| .pdf | 2 | 0 % |
| use | 2 | 0 % |
| caltec | 2 | 0 % |
| fourth | 2 | 0 % |
| university | 2 | 0 % |
| n | 2 | 0 % |
| 36 | 2 | 0 % |
| principle | 2 | 0 % |
| rouse | 2 | 0 % |
| results | 2 | 0 % |
| takahashi | 2 | 0 % |
| formation | 2 | 0 % |
| dynamic | 2 | 0 % |
| 0.25 | 2 | 0 % |
| logvinovich | 2 | 0 % |
| supercavitation-problems | 2 | 0 % |
| integral | 2 | 0 % |
| modelling | 2 | 0 % |
| noozle | 2 | 0 % |
| navier | 2 | 0 % |
| mixed | 2 | 0 % |
| single-hole | 2 | 0 % |
| substrack | 2 | 0 % |
| valve | 2 | 0 % |
| gosman | 2 | 0 % |
| head | 2 | 0 % |
| d. | 2 | 0 % |
| eno | 2 | 0 % |
| beijing | 2 | 0 % |
| s | 2 | 0 % |
| lauterborn | 2 | 0 % |
| definition | 2 | 0 % |
| takahira | 2 | 0 % |
| boat | 2 | 0 % |
| farhat | 2 | 0 % |
| nitrogen | 2 | 0 % |
| around | 2 | 0 % |
| potential | 2 | 0 % |
| machinery | 2 | 0 % |
| sharp | 2 | 0 % |
| 2d | 2 | 0 % |
| phd | 2 | 0 % |
| tools | 2 | 0 % |
| kuiper | 2 | 0 % |
| tip-vortex | 2 | 0 % |
| circular | 2 | 0 % |
| schiebe | 2 | 0 % |
| robert | 2 | 0 % |
| standard | 2 | 0 % |
| usa | 2 | 0 % |
| kei | 2 | 0 % |
| rotor | 2 | 0 % |
| hammer | 2 | 0 % |
| report | 2 | 0 % |
| dumont | 2 | 0 % |
| abstract | 2 | 0 % |
| submerged | 2 | 0 % |
| kuklinski | 2 | 0 % |
| velocity-pressure | 2 | 0 % |
| transparent | 2 | 0 % |
| stop | 2 | 0 % |
| 3 | 2 | 0 % |
| slender | 2 | 0 % |
| rolla | 2 | 0 % |
| equals | 1 | 0 % |
| philos | 1 | 0 % |
| loading.pdf | 1 | 0 % |
| kubato | 1 | 0 % |
| controllable | 1 | 0 % |
| finite | 1 | 0 % |
| ita | 1 | 0 % |
| load | 1 | 0 % |
| fastcam | 1 | 0 % |
| hlpa | 1 | 0 % |
| tested | 1 | 0 % |
| subject | 1 | 0 % |
| constrained | 1 | 0 % |
| ville | 1 | 0 % |
| cav2001. | 1 | 0 % |
| lord | 1 | 0 % |
| pitting | 1 | 0 % |
| moment | 1 | 0 % |
| sounds | 1 | 0 % |
| emerson | 1 | 0 % |
| equilibrium | 1 | 0 % |
| figure | 1 | 0 % |
| scaling | 1 | 0 % |
| tomita | 1 | 0 % |
| wall | 1 | 0 % |
| penetration | 1 | 0 % |
| mirror | 1 | 0 % |
| regimes | 1 | 0 % |
| rule | 1 | 0 % |
| restrictor | 1 | 0 % |
| turning | 1 | 0 % |
| bernouli | 1 | 0 % |
| press | 1 | 0 % |
| qsou | 1 | 0 % |
| bernoulli | 1 | 0 % |
| sumulations | 1 | 0 % |
| jets | 1 | 0 % |
| procedure | 1 | 0 % |
| panasonic | 1 | 0 % |
| plastics | 1 | 0 % |
| ganippa | 1 | 0 % |
| explained | 1 | 0 % |
| can | 1 | 0 % |
| curves | 1 | 0 % |
| 8080/dp9/getrecord/oai_dc/cav2001.oai/oai | 1 | 0 % |
| derived | 1 | 0 % |
| virtual | 1 | 0 % |
| prop | 1 | 0 % |
| furuya | 1 | 0 % |
| choked | 1 | 0 % |
| qian | 1 | 0 % |
| analyzer | 1 | 0 % |
| nasa | 1 | 0 % |
| dyno | 1 | 0 % |
| recovery | 1 | 0 % |
| munition | 1 | 0 % |
| volutes | 1 | 0 % |
| compressible-flow | 1 | 0 % |
| coefficients | 1 | 0 % |
| dang | 1 | 0 % |
| plates | 1 | 0 % |
| eguzquiza | 1 | 0 % |
| tech | 1 | 0 % |
| pond | 1 | 0 % |
| circulating | 1 | 0 % |
| valves;pdf | 1 | 0 % |
| nucleation | 1 | 0 % |
| hall | 1 | 0 % |
| computational | 1 | 0 % |
| preece | 1 | 0 % |
| propeller-hull-vortex | 1 | 0 % |
| algorithms | 1 | 0 % |
| astolfi | 1 | 0 % |
| sweep | 1 | 0 % |
| analysis. | 1 | 0 % |
| cav2001.library.caltech.edu | 1 | 0 % |
| problem | 1 | 0 % |
| smith | 1 | 0 % |
| proceedings | 1 | 0 % |
| moving | 1 | 0 % |
| knapp | 1 | 0 % |
| spilled | 1 | 0 % |
| mohamed | 1 | 0 % |
| pelton | 1 | 0 % |
| fps | 1 | 0 % |
| 1992 | 1 | 0 % |
| focused | 1 | 0 % |
| compounder | 1 | 0 % |
| transducer | 1 | 0 % |
| supersynchronous | 1 | 0 % |
| solid | 1 | 0 % |
| nonequilibrium | 1 | 0 % |
| propulsor | 1 | 0 % |
| orific | 1 | 0 % |
| flowmeter | 1 | 0 % |
| dependence | 1 | 0 % |
| rate | 1 | 0 % |
| measured | 1 | 0 % |
| numachi | 1 | 0 % |
| rayleigh-plesset n-s | 1 | 0 % |
| degased | 1 | 0 % |
| impulse | 1 | 0 % |
| piping | 1 | 0 % |
| change | 1 | 0 % |
| r.t | 1 | 0 % |
| strong | 1 | 0 % |
| nonlifting | 1 | 0 % |
| henda | 1 | 0 % |
| diers | 1 | 0 % |
| spillways | 1 | 0 % |
| conditions | 1 | 0 % |
| sedov | 1 | 0 % |
| california | 1 | 0 % |
| measuring | 1 | 0 % |
| tsujimoto | 1 | 0 % |
| simples | 1 | 0 % |
| ratio | 1 | 0 % |
| frequencies | 1 | 0 % |
| surface-tension | 1 | 0 % |
| ellipsoid | 1 | 0 % |
| solved | 1 | 0 % |
| ca | 1 | 0 % |
| schoon | 1 | 0 % |
| j-l. | 1 | 0 % |
| fluidized | 1 | 0 % |
| compressor | 1 | 0 % |
| rupture | 1 | 0 % |
| pressures | 1 | 0 % |
| yoshiaki | 1 | 0 % |
| correctly | 1 | 0 % |
| produce | 1 | 0 % |
| integrated | 1 | 0 % |
| mcnown | 1 | 0 % |
| pitch | 1 | 0 % |
| sa | 1 | 0 % |
| érosion | 1 | 0 % |
| 100 | 1 | 0 % |
| b. | 1 | 0 % |
| 300 | 1 | 0 % |
| stress | 1 | 0 % |
| show | 1 | 0 % |
| furst | 1 | 0 % |
| bell | 1 | 0 % |
| parameter | 1 | 0 % |
| associated | 1 | 0 % |
| cl | 1 | 0 % |
| uncertainty | 1 | 0 % |
| wing | 1 | 0 % |
| toyota | 1 | 0 % |
| 40000 | 1 | 0 % |
| centrifuge | 1 | 0 % |
| contact | 1 | 0 % |
| dead | 1 | 0 % |
| gary | 1 | 0 % |
| multiperforated | 1 | 0 % |
| interpretation | 1 | 0 % |
| machine | 1 | 0 % |
| approximation | 1 | 0 % |
| heymann | 1 | 0 % |
| crash-stop | 1 | 0 % |
| invaders | 1 | 0 % |
| original | 1 | 0 % |
| dams | 1 | 0 % |
| he | 1 | 0 % |
| compounds | 1 | 0 % |
| behavior | 1 | 0 % |
| meyer | 1 | 0 % |
| cold | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| marscher | 1 | 0 % |
| relations | 1 | 0 % |
| technical | 1 | 0 % |
| repro | 1 | 0 % |
| williams | 1 | 0 % |
| ultrasonics | 1 | 0 % |
| aggressiveness | 1 | 0 % |
| regiane | 1 | 0 % |
| injectors | 1 | 0 % |
| due | 1 | 0 % |
| princeton | 1 | 0 % |
| lubricant | 1 | 0 % |
| soyama | 1 | 0 % |
| kerwin | 1 | 0 % |
| related | 1 | 0 % |
| roll-up | 1 | 0 % |
| mccormick | 1 | 0 % |
| download | 1 | 0 % |
| small | 1 | 0 % |
| alloys | 1 | 0 % |
| spectral | 1 | 0 % |
| six | 1 | 0 % |
| visualization | 1 | 0 % |
| billet | 1 | 0 % |
| dimensional | 1 | 0 % |
| meters | 1 | 0 % |
| amplitude | 1 | 0 % |
| patella | 1 | 0 % |
| modelization | 1 | 0 % |
| oxidize | 1 | 0 % |
| freestream | 1 | 0 % |
| hydrodynamics | 1 | 0 % |
| cavitators | 1 | 0 % |
| cascade | 1 | 0 % |
| g. | 1 | 0 % |
| tendency | 1 | 0 % |
| hovercraft | 1 | 0 % |
| sampling | 1 | 0 % |
| index | 1 | 0 % |
| multi-phase | 1 | 0 % |
| length | 1 | 0 % |
| notes | 1 | 0 % |
| tunel | 1 | 0 % |
| pellone | 1 | 0 % |
| propcav | 1 | 0 % |
| intensity | 1 | 0 % |
| square | 1 | 0 % |
| bladed | 1 | 0 % |
| validative | 1 | 0 % |
| matrix | 1 | 0 % |
| .85-80 | 1 | 0 % |
| non-circular | 1 | 0 % |
| hydrofoils | 1 | 0 % |
| webkr | 1 | 0 % |
| valves | 1 | 0 % |
| template | 1 | 0 % |
| circle | 1 | 0 % |
| ohan | 1 | 0 % |
| overview | 1 | 0 % |
| parameters | 1 | 0 % |
| tension | 1 | 0 % |
| hitch-hikers | 1 | 0 % |
| bypass | 1 | 0 % |
| skewed | 1 | 0 % |
| azimutal | 1 | 0 % |
| impact | 1 | 0 % |
| guage | 1 | 0 % |
| parallell | 1 | 0 % |
| same | 1 | 0 % |
| eddy | 1 | 0 % |
| arl | 1 | 0 % |
| calibration | 1 | 0 % |
| unsteadiness | 1 | 0 % |
| specification | 1 | 0 % |
| wedge | 1 | 0 % |
| tanks | 1 | 0 % |
| papers | 1 | 0 % |
| sassanelli | 1 | 0 % |
| beaker | 1 | 0 % |
| torpedo | 1 | 0 % |
| sujimoto | 1 | 0 % |
| features | 1 | 0 % |
| jessup | 1 | 0 % |
| through | 1 | 0 % |
| oil | 1 | 0 % |
| symmetry | 1 | 0 % |
| hydralic | 1 | 0 % |
| nanomizer | 1 | 0 % |
| reliability | 1 | 0 % |
| rise | 1 | 0 % |
| mechatronic | 1 | 0 % |
| table | 1 | 0 % |
| non-spherical | 1 | 0 % |
| droplet | 1 | 0 % |
| seperation | 1 | 0 % |
| naca-66 | 1 | 0 % |
| eulerian/lagrangian | 1 | 0 % |
| clusters | 1 | 0 % |
| hess | 1 | 0 % |
| its | 1 | 0 % |
| undersea | 1 | 0 % |
| gaussian | 1 | 0 % |
| line | 1 | 0 % |
| property | 1 | 0 % |
| utilization | 1 | 0 % |
| benoit | 1 | 0 % |
| similarity | 1 | 0 % |
| gotfred | 1 | 0 % |
| focussing | 1 | 0 % |
| coeffecient | 1 | 0 % |
| arc.cs.odu.edu | 1 | 0 % |
| some | 1 | 0 % |
| recirculation | 1 | 0 % |
| akishima | 1 | 0 % |
| signs | 1 | 0 % |
| ballast | 1 | 0 % |
| detection | 1 | 0 % |
| zone | 1 | 0 % |
| bearing | 1 | 0 % |
| motor | 1 | 0 % |
| a8 | 1 | 0 % |
| foreward | 1 | 0 % |
| coutier | 1 | 0 % |
| rans | 1 | 0 % |
| maines | 1 | 0 % |
| transfer | 1 | 0 % |
| film | 1 | 0 % |
| graham | 1 | 0 % |
| asurface | 1 | 0 % |
| chorin | 1 | 0 % |
| visualisation | 1 | 0 % |
| 2000-01-1799 | 1 | 0 % |
| caltech. | 1 | 0 % |
| 1994 | 1 | 0 % |
| constant | 1 | 0 % |
| techniques | 1 | 0 % |
| 1988 | 1 | 0 % |
| large | 1 | 0 % |
| berntsen | 1 | 0 % |
| lithotripsy | 1 | 0 % |
| vessel | 1 | 0 % |
| non | 1 | 0 % |
| highspeed | 1 | 0 % |
| deviation | 1 | 0 % |
| does | 1 | 0 % |
| organic | 1 | 0 % |
| camara | 1 | 0 % |
| derivication | 1 | 0 % |
| fortes | 1 | 0 % |
| mitsui | 1 | 0 % |
| passive | 1 | 0 % |
| dissolved-gas | 1 | 0 % |
| solver | 1 | 0 % |
| solve | 1 | 0 % |
| principal | 1 | 0 % |
| research | 1 | 0 % |
| young | 1 | 0 % |
| solutions | 1 | 0 % |
| spiral | 1 | 0 % |
| between | 1 | 0 % |
| sensitive | 1 | 0 % |
| boundaries | 1 | 0 % |
| 102 | 1 | 0 % |
| techonogy | 1 | 0 % |
| aluminium | 1 | 0 % |
| power | 1 | 0 % |
| elastic | 1 | 0 % |
| re-entrant | 1 | 0 % |
| positive | 1 | 0 % |
| “similarities | 1 | 0 % |
| set-up | 1 | 0 % |
| seaplane | 1 | 0 % |
| attack | 1 | 0 % |
| wvd | 1 | 0 % |
| dispersion | 1 | 0 % |
| 1999-01-0524 | 1 | 0 % |
| formed? | 1 | 0 % |
| torsion | 1 | 0 % |
| extract | 1 | 0 % |
| stability | 1 | 0 % |
| orlando | 1 | 0 % |
| nnnxn | 1 | 0 % |
| kalumuck | 1 | 0 % |
| no | 1 | 0 % |
| france | 1 | 0 % |
| zhu | 1 | 0 % |
| piv | 1 | 0 % |
| hsmac | 1 | 0 % |
| colonius | 1 | 0 % |
| js | 1 | 0 % |
| skewed propeller | 1 | 0 % |
| sweden | 1 | 0 % |
| object | 1 | 0 % |
| rautenberg | 1 | 0 % |
| inertia | 1 | 0 % |
| petroleum | 1 | 0 % |
| stimulating | 1 | 0 % |
| boncinelli | 1 | 0 % |
| x-ray | 1 | 0 % |
| pattern | 1 | 0 % |
| complete | 1 | 0 % |
| studying | 1 | 0 % |
| balancing | 1 | 0 % |
| kato | 1 | 0 % |
| content | 1 | 0 % |
| behaviour | 1 | 0 % |
| j-franc | 1 | 0 % |
| mie-grüneisen | 1 | 0 % |
| negative | 1 | 0 % |
| takahide | 1 | 0 % |
| behind | 1 | 0 % |
| specific | 1 | 0 % |
| computers | 1 | 0 % |
| badock | 1 | 0 % |
| osaka | 1 | 0 % |
| sections | 1 | 0 % |
| m. | 1 | 0 % |
| continuity | 1 | 0 % |
| maneuver | 1 | 0 % |
| shaped | 1 | 0 % |
| irrotational | 1 | 0 % |
| detrmine | 1 | 0 % |
| et | 1 | 0 % |
| matsumoto | 1 | 0 % |
| prevention | 1 | 0 % |
| depth | 1 | 0 % |
| iahr | 1 | 0 % |
| boundries | 1 | 0 % |
| vwo | 1 | 0 % |
| prentice | 1 | 0 % |
| venturi | 1 | 0 % |
| chemicals | 1 | 0 % |
| francis | 1 | 0 % |
| sets | 1 | 0 % |
| gauge | 1 | 0 % |
| wallis | 1 | 0 % |
| turbulence | 1 | 0 % |
| diagrama | 1 | 0 % |
| paolo | 1 | 0 % |
| distributed | 1 | 0 % |
| delale | 1 | 0 % |
| deformed | 1 | 0 % |
| lubrication | 1 | 0 % |
| view | 1 | 0 % |
| grids | 1 | 0 % |
| curvature | 1 | 0 % |
| 2008 | 1 | 0 % |
| properties | 1 | 0 % |
| open | 1 | 0 % |
| clearance | 1 | 0 % |
| philipe | 1 | 0 % |
| forms | 1 | 0 % |
| torque | 1 | 0 % |
| throttling | 1 | 0 % |
| radial | 1 | 0 % |
| lu | 1 | 0 % |
| crash | 1 | 0 % |
| exit | 1 | 0 % |
| natural | 1 | 0 % |
| 2 | 1 | 0 % |
| philippe | 1 | 0 % |
| marin | 1 | 0 % |
| vane | 1 | 0 % |
| restriction | 1 | 0 % |
| stream | 1 | 0 % |
| pierre | 1 | 0 % |
| johannes | 1 | 0 % |
| b-h | 1 | 0 % |
| partial | 1 | 0 % |
| sokhotski-plemelj | 1 | 0 % |
| bearings | 1 | 0 % |
| rig | 1 | 0 % |
| localized | 1 | 0 % |
| dynamometer | 1 | 0 % |
| yury | 1 | 0 % |
| parsons | 1 | 0 % |
| 1st | 1 | 0 % |
| cpp | 1 | 0 % |
| luminescence | 1 | 0 % |
| affected | 1 | 0 % |
| hydrophone | 1 | 0 % |
| vaporous | 1 | 0 % |
| micro | 1 | 0 % |
| removal | 1 | 0 % |
| efros | 1 | 0 % |
| applications. | 1 | 0 % |
| weak | 1 | 0 % |
| keller | 1 | 0 % |
| oxforde | 1 | 0 % |
| level | 1 | 0 % |
| simple | 1 | 0 % |
| 6.7 | 1 | 0 % |
| free-shear | 1 | 0 % |
| jet-modelling | 1 | 0 % |
| shima | 1 | 0 % |
| pogo | 1 | 0 % |
| homogeneous | 1 | 0 % |
| sea | 1 | 0 % |
| harmonic | 1 | 0 % |
| hill | 1 | 0 % |
| craft | 1 | 0 % |
| media | 1 | 0 % |
| 1998 | 1 | 0 % |
| cav2dbl | 1 | 0 % |
| advance | 1 | 0 % |
| r | 1 | 0 % |
| straight | 1 | 0 % |
| barotropic | 1 | 0 % |
| studies | 1 | 0 % |
| cluster | 1 | 0 % |
| hykat | 1 | 0 % |
| diameter | 1 | 0 % |
| leakage | 1 | 0 % |
| snapshots | 1 | 0 % |
| Other words | 194 | 4.3 % |
|