| 1504 different keywords | Search | Percent |
|---|
| cavitation | 449 | 7.4 % |
| of | 213 | 3.5 % |
| in | 110 | 1.8 % |
| pdf | 104 | 1.7 % |
| orifice | 101 | 1.6 % |
| propeller | 97 | 1.6 % |
| and | 95 | 1.5 % |
| pump | 84 | 1.3 % |
| on | 69 | 1.1 % |
| vortex | 67 | 1.1 % |
| a | 63 | 1 % |
| restriction | 62 | 1 % |
| flow | 52 | 0.8 % |
| the | 51 | 0.8 % |
| fluent | 47 | 0.7 % |
| filetype | 46 | 0.7 % |
| centrifugal | 43 | 0.7 % |
| water | 40 | 0.6 % |
| pressure | 37 | 0.6 % |
| bubble | 36 | 0.5 % |
| simulation | 36 | 0.5 % |
| model | 34 | 0.5 % |
| supercavitation | 34 | 0.5 % |
| for | 34 | 0.5 % |
| turbine | 32 | 0.5 % |
| cavitating | 32 | 0.5 % |
| kaplan | 30 | 0.4 % |
| inducer | 29 | 0.4 % |
| noise | 29 | 0.4 % |
| numerical | 27 | 0.4 % |
| analysis | 26 | 0.4 % |
| design | 26 | 0.4 % |
| ship | 26 | 0.4 % |
| study | 25 | 0.4 % |
| tip | 25 | 0.4 % |
| number | 24 | 0.3 % |
| jet | 23 | 0.3 % |
| rudder | 22 | 0.3 % |
| experimental | 22 | 0.3 % |
| dynamics | 21 | 0.3 % |
| surface | 21 | 0.3 % |
| to | 21 | 0.3 % |
| tunnel | 21 | 0.3 % |
| method | 21 | 0.3 % |
| pumps | 20 | 0.3 % |
| suction | 20 | 0.3 % |
| nozzle | 20 | 0.3 % |
| test | 19 | 0.3 % |
| erosion | 19 | 0.3 % |
| hydrofoil | 19 | 0.3 % |
| effect | 19 | 0.3 % |
| supercavitating | 18 | 0.2 % |
| naca | 18 | 0.2 % |
| cavity | 18 | 0.2 % |
| calculation | 18 | 0.2 % |
| effects | 18 | 0.2 % |
| marine | 17 | 0.2 % |
| bubbles | 17 | 0.2 % |
| with | 17 | 0.2 % |
| velocity | 17 | 0.2 % |
| frequency | 17 | 0.2 % |
| sheet | 16 | 0.2 % |
| author | 15 | 0.2 % |
| by | 15 | 0.2 % |
| boundary | 15 | 0.2 % |
| types | 15 | 0.2 % |
| cav2001 | 15 | 0.2 % |
| propellers | 15 | 0.2 % |
| orifices | 15 | 0.2 % |
| blade | 14 | 0.2 % |
| cfd | 14 | 0.2 % |
| intitle | 13 | 0.2 % |
| flows | 13 | 0.2 % |
| paper | 13 | 0.2 % |
| rocket | 13 | 0.2 % |
| modeling | 13 | 0.2 % |
| diesel | 13 | 0.2 % |
| equation | 13 | 0.2 % |
| fluid | 12 | 0.1 % |
| journal | 12 | 0.1 % |
| size | 12 | 0.1 % |
| piercing | 12 | 0.1 % |
| scale | 11 | 0.1 % |
| & | 11 | 0.1 % |
| hydrodynamic | 11 | 0.1 % |
| turbopump | 10 | 0.1 % |
| panel | 10 | 0.1 % |
| butterfly | 10 | 0.1 % |
| acoustic | 10 | 0.1 % |
| large | 10 | 0.1 % |
| characteristics | 10 | 0.1 % |
| prediction | 10 | 0.1 % |
| dynamic | 10 | 0.1 % |
| 2d | 10 | 0.1 % |
| high | 10 | 0.1 % |
| super | 9 | 0.1 % |
| experiment | 9 | 0.1 % |
| rayleigh-plesset | 9 | 0.1 % |
| sheet/cloud | 9 | 0.1 % |
| unsteady | 9 | 0.1 % |
| liquid | 9 | 0.1 % |
| eddy | 9 | 0.1 % |
| ventilated | 9 | 0.1 % |
| 3d | 9 | 0.1 % |
| speed | 9 | 0.1 % |
| plate | 9 | 0.1 % |
| vibration | 9 | 0.1 % |
| hole | 9 | 0.1 % |
| valve | 9 | 0.1 % |
| joint | 9 | 0.1 % |
| horn | 8 | 0.1 % |
| vof | 8 | 0.1 % |
| collapse | 8 | 0.1 % |
| performance | 8 | 0.1 % |
| 2001 | 8 | 0.1 % |
| quality | 8 | 0.1 % |
| cascade | 8 | 0.1 % |
| free | 8 | 0.1 % |
| turbines | 8 | 0.1 % |
| turbomachinery | 8 | 0.1 % |
| force | 8 | 0.1 % |
| mechanism | 8 | 0.1 % |
| international | 8 | 0.1 % |
| head | 8 | 0.1 % |
| induced | 8 | 0.1 % |
| cav | 8 | 0.1 % |
| plesset | 8 | 0.1 % |
| hydraulic | 8 | 0.1 % |
| nexearch | 8 | 0.1 % |
| what | 7 | 0.1 % |
| underwater | 7 | 0.1 % |
| solid | 7 | 0.1 % |
| video | 7 | 0.1 % |
| symposium | 7 | 0.1 % |
| laser | 7 | 0.1 % |
| how | 7 | 0.1 % |
| is | 7 | 0.1 % |
| similarity | 7 | 0.1 % |
| time-frequency | 7 | 0.1 % |
| wake | 7 | 0.1 % |
| an | 7 | 0.1 % |
| time | 7 | 0.1 % |
| compressibility | 7 | 0.1 % |
| cavities | 7 | 0.1 % |
| two | 7 | 0.1 % |
| phase | 6 | 0 % |
| inlet | 6 | 0 % |
| drag | 6 | 0 % |
| injector | 6 | 0 % |
| series | 6 | 0 % |
| pipe | 6 | 0 % |
| emission | 6 | 0 % |
| formula | 6 | 0 % |
| thermal | 6 | 0 % |
| introduction | 6 | 0 % |
| stokes | 6 | 0 % |
| bearing | 6 | 0 % |
| sizing | 6 | 0 % |
| solution | 6 | 0 % |
| sae | 6 | 0 % |
| compressible | 6 | 0 % |
| example | 6 | 0 % |
| vladimir | 6 | 0 % |
| thesis | 6 | 0 % |
| 0015 | 6 | 0 % |
| senocak | 6 | 0 % |
| wave | 6 | 0 % |
| single | 6 | 0 % |
| methods | 6 | 0 % |
| downstream | 6 | 0 % |
| forces | 6 | 0 % |
| shyy | 6 | 0 % |
| navier | 6 | 0 % |
| ... | 6 | 0 % |
| around | 6 | 0 % |
| cavitations | 6 | 0 % |
| inception | 6 | 0 % |
| air | 6 | 0 % |
| caviation | 5 | 0 % |
| n. | 5 | 0 % |
| projectile | 5 | 0 % |
| measurement | 5 | 0 % |
| aiaa | 5 | 0 % |
| procedure | 5 | 0 % |
| navier-stokes | 5 | 0 % |
| rate | 5 | 0 % |
| intake | 5 | 0 % |
| state | 5 | 0 % |
| artificial | 5 | 0 % |
| pitch | 5 | 0 % |
| models | 5 | 0 % |
| axial | 5 | 0 % |
| oscillation | 5 | 0 % |
| sound | 5 | 0 % |
| hull | 5 | 0 % |
| distribution | 5 | 0 % |
| rotating | 5 | 0 % |
| through | 5 | 0 % |
| foil | 5 | 0 % |
| vessel | 5 | 0 % |
| interaction | 5 | 0 % |
| npsh | 5 | 0 % |
| injection | 5 | 0 % |
| development | 5 | 0 % |
| axisymmetric | 5 | 0 % |
| semenenko | 5 | 0 % |
| .pdf | 5 | 0 % |
| venturi | 5 | 0 % |
| stoffel | 5 | 0 % |
| turbulence | 5 | 0 % |
| conclusion | 5 | 0 % |
| w. | 5 | 0 % |
| investigation | 5 | 0 % |
| 2 | 5 | 0 % |
| growth | 5 | 0 % |
| supercavity | 5 | 0 % |
| song | 5 | 0 % |
| submerged | 5 | 0 % |
| rayleigh | 5 | 0 % |
| at | 5 | 0 % |
| structure | 5 | 0 % |
| multi | 5 | 0 % |
| form | 4 | 0 % |
| cs | 4 | 0 % |
| incipient | 4 | 0 % |
| azipod | 4 | 0 % |
| runner | 4 | 0 % |
| heat | 4 | 0 % |
| lift | 4 | 0 % |
| i. | 4 | 0 % |
| ratio | 4 | 0 % |
| ittc | 4 | 0 % |
| instability | 4 | 0 % |
| nuclei | 4 | 0 % |
| liquids | 4 | 0 % |
| wing | 4 | 0 % |
| 1991 | 4 | 0 % |
| technical | 4 | 0 % |
| reentrant | 4 | 0 % |
| flow | 4 | 0 % |
| piuctures | 4 | 0 % |
| 1983 | 4 | 0 % |
| savchenko | 4 | 0 % |
| dimensional | 4 | 0 % |
| coefficient | 4 | 0 % |
| propellering | 4 | 0 % |
| impact | 4 | 0 % |
| surge | 4 | 0 % |
| inducers | 4 | 0 % |
| b | 4 | 0 % |
| arndt | 4 | 0 % |
| reynolds | 4 | 0 % |
| application | 4 | 0 % |
| boundaries | 4 | 0 % |
| waves | 4 | 0 % |
| - | 4 | 0 % |
| exhibit | 4 | 0 % |
| predictions | 4 | 0 % |
| maneuvering | 4 | 0 % |
| behaviour | 4 | 0 % |
| element | 4 | 0 % |
| shock | 4 | 0 % |
| spray | 4 | 0 % |
| using | 4 | 0 % |
| thoma | 4 | 0 % |
| signal | 4 | 0 % |
| rudders | 4 | 0 % |
| new | 4 | 0 % |
| matsumoto | 4 | 0 % |
| imfo | 4 | 0 % |
| throat | 4 | 0 % |
| blades | 4 | 0 % |
| volume | 4 | 0 % |
| airfoil | 4 | 0 % |
| sessionb9.001 | 4 | 0 % |
| logvinovich | 4 | 0 % |
| gas | 4 | 0 % |
| spectrum | 4 | 0 % |
| conf. | 4 | 0 % |
| franc | 4 | 0 % |
| vehicle | 4 | 0 % |
| grekula | 4 | 0 % |
| solids | 4 | 0 % |
| ships | 4 | 0 % |
| from | 4 | 0 % |
| qin | 4 | 0 % |
| near | 4 | 0 % |
| barotropic | 4 | 0 % |
| diameter | 4 | 0 % |
| dual | 3 | 0 % |
| shapes | 3 | 0 % |
| constrained | 3 | 0 % |
| used | 3 | 0 % |
| energy | 3 | 0 % |
| scaling | 3 | 0 % |
| system | 3 | 0 % |
| prop | 3 | 0 % |
| sauer | 3 | 0 % |
| static | 3 | 0 % |
| plates | 3 | 0 % |
| different | 3 | 0 % |
| type | 3 | 0 % |
| german | 3 | 0 % |
| c. | 3 | 0 % |
| hydrauliques | 3 | 0 % |
| conditions | 3 | 0 % |
| measuring | 3 | 0 % |
| institute | 3 | 0 % |
| rotational | 3 | 0 % |
| mass | 3 | 0 % |
| bell | 3 | 0 % |
| bodies | 3 | 0 % |
| behavior | 3 | 0 % |
| williams | 3 | 0 % |
| over | 3 | 0 % |
| amplitude | 3 | 0 % |
| hydrodynamics | 3 | 0 % |
| prevent | 3 | 0 % |
| pasadena | 3 | 0 % |
| length | 3 | 0 % |
| cavitator | 3 | 0 % |
| propellor | 3 | 0 % |
| asme | 3 | 0 % |
| molecular | 3 | 0 % |
| bernd | 3 | 0 % |
| line | 3 | 0 % |
| layer | 3 | 0 % |
| atomization | 3 | 0 % |
| measurements | 3 | 0 % |
| propulsion | 3 | 0 % |
| motion | 3 | 0 % |
| dissolved | 3 | 0 % |
| hydro | 3 | 0 % |
| investigations | 3 | 0 % |
| atlar | 3 | 0 % |
| field | 3 | 0 % |
| process | 3 | 0 % |
| theory | 3 | 0 % |
| engine | 3 | 0 % |
| working | 3 | 0 % |
| phenomenon | 3 | 0 % |
| turbulent | 3 | 0 % |
| numeca | 3 | 0 % |
| comparison | 3 | 0 % |
| generation | 3 | 0 % |
| stability | 3 | 0 % |
| les | 3 | 0 % |
| zwick | 3 | 0 % |
| tank | 3 | 0 % |
| data | 3 | 0 % |
| casing | 3 | 0 % |
| impeller | 3 | 0 % |
| spherical | 3 | 0 % |
| barnaby | 3 | 0 % |
| control | 3 | 0 % |
| boncinelli | 3 | 0 % |
| pattern | 3 | 0 % |
| fully | 3 | 0 % |
| o | 3 | 0 % |
| apparatus | 3 | 0 % |
| ultrasound | 3 | 0 % |
| problems | 3 | 0 % |
| abs | 3 | 0 % |
| hosangadi | 3 | 0 % |
| approach | 3 | 0 % |
| reichardt | 3 | 0 % |
| critical | 3 | 0 % |
| darmstadt | 3 | 0 % |
| francis | 3 | 0 % |
| paolo | 3 | 0 % |
| relative | 3 | 0 % |
| escaler | 3 | 0 % |
| clearance | 3 | 0 % |
| modelling | 3 | 0 % |
| fields | 3 | 0 % |
| japan | 3 | 0 % |
| schnerr | 3 | 0 % |
| turbo | 3 | 0 % |
| a. | 3 | 0 % |
| generated | 3 | 0 % |
| stream | 3 | 0 % |
| full | 3 | 0 % |
| rig | 3 | 0 % |
| farhat | 3 | 0 % |
| testing | 3 | 0 % |
| phd | 3 | 0 % |
| keller | 3 | 0 % |
| installation | 3 | 0 % |
| 1925 | 3 | 0 % |
| dissertation | 3 | 0 % |
| material | 3 | 0 % |
| media | 3 | 0 % |
| advance | 3 | 0 % |
| straight | 3 | 0 % |
| leakage | 3 | 0 % |
| mach | 2 | 0 % |
| finite | 2 | 0 % |
| light | 2 | 0 % |
| materials | 2 | 0 % |
| 1989 | 2 | 0 % |
| 4th | 2 | 0 % |
| jets | 2 | 0 % |
| rankine | 2 | 0 % |
| curves | 2 | 0 % |
| yoshiki | 2 | 0 % |
| lab | 2 | 0 % |
| analyzer | 2 | 0 % |
| helical | 2 | 0 % |
| k | 2 | 0 % |
| tech | 2 | 0 % |
| nucleation | 2 | 0 % |
| astolfi | 2 | 0 % |
| project | 2 | 0 % |
| ujf | 2 | 0 % |
| coutier-delgosha | 2 | 0 % |
| problem | 2 | 0 % |
| mechanics | 2 | 0 % |
| 23 | 2 | 0 % |
| software | 2 | 0 % |
| vortices | 2 | 0 % |
| farrell | 2 | 0 % |
| excitation | 2 | 0 % |
| safl | 2 | 0 % |
| gate | 2 | 0 % |
| perspectives | 2 | 0 % |
| kam | 2 | 0 % |
| piping | 2 | 0 % |
| partially | 2 | 0 % |
| affect | 2 | 0 % |
| kavitation | 2 | 0 % |
| joussellin | 2 | 0 % |
| naca0015 | 2 | 0 % |
| j-farrell | 2 | 0 % |
| local | 2 | 0 % |
| case | 2 | 0 % |
| conservative | 2 | 0 % |
| transducers | 2 | 0 % |
| mouth | 2 | 0 % |
| plk | 2 | 0 % |
| ellipsoid | 2 | 0 % |
| thickness | 2 | 0 % |
| theoratical | 2 | 0 % |
| mcnown | 2 | 0 % |
| mesh | 2 | 0 % |
| phantom | 2 | 0 % |
| stress | 2 | 0 % |
| similarities | 2 | 0 % |
| mpuf-3a | 2 | 0 % |
| ring | 2 | 0 % |
| de | 2 | 0 % |
| relation | 2 | 0 % |
| away | 2 | 0 % |
| stabilized | 2 | 0 % |
| rules | 2 | 0 % |
| s15c | 2 | 0 % |
| olivier | 2 | 0 % |
| mehmet | 2 | 0 % |
| vasin | 2 | 0 % |
| original | 2 | 0 % |
| larry | 2 | 0 % |
| far | 2 | 0 % |
| required | 2 | 0 % |
| naca66 | 2 | 0 % |
| fine | 2 | 0 % |
| due | 2 | 0 % |
| sump | 2 | 0 % |
| laser-produced | 2 | 0 % |
| download | 2 | 0 % |
| la | 2 | 0 % |
| delannoy | 2 | 0 % |
| prosperetti | 2 | 0 % |
| lecture | 2 | 0 % |
| astm | 2 | 0 % |
| index | 2 | 0 % |
| ng | 2 | 0 % |
| tunel | 2 | 0 % |
| oscillating | 2 | 0 % |
| conform | 2 | 0 % |
| model-scale | 2 | 0 % |
| bevel | 2 | 0 % |
| valves | 2 | 0 % |
| c | 2 | 0 % |
| bruin | 2 | 0 % |
| maintenance | 2 | 0 % |
| surface-piercing | 2 | 0 % |
| caracteristics | 2 | 0 % |
| anti | 2 | 0 % |
| m | 2 | 0 % |
| oil | 2 | 0 % |
| hattori | 2 | 0 % |
| ballistics | 2 | 0 % |
| rise | 2 | 0 % |
| seawater | 2 | 0 % |
| table | 2 | 0 % |
| that | 2 | 0 % |
| green | 2 | 0 % |
| differential | 2 | 0 % |
| its | 2 | 0 % |
| no.2.pp.92-101 | 2 | 0 % |
| 5-blade | 2 | 0 % |
| developed | 2 | 0 % |
| propelers | 2 | 0 % |
| allintitle | 2 | 0 % |
| 300mm | 2 | 0 % |
| function | 2 | 0 % |
| added | 2 | 0 % |
| channel | 2 | 0 % |
| lithotriptor | 2 | 0 % |
| spectrometer | 2 | 0 % |
| transfer | 2 | 0 % |
| improvement | 2 | 0 % |
| david | 2 | 0 % |
| sakoda | 2 | 0 % |
| location | 2 | 0 % |
| ioannides | 2 | 0 % |
| zhong | 2 | 0 % |
| pod | 2 | 0 % |
| microbubbles | 2 | 0 % |
| intakes | 2 | 0 % |
| between | 2 | 0 % |
| videos | 2 | 0 % |
| vs | 2 | 0 % |
| measure | 2 | 0 % |
| you | 2 | 0 % |
| parallel | 2 | 0 % |
| lemonnier | 2 | 0 % |
| electric-explosion | 2 | 0 % |
| olofsson | 2 | 0 % |
| j. | 2 | 0 % |
| chamber | 2 | 0 % |
| re-entrant | 2 | 0 % |
| technology | 2 | 0 % |
| flows | 2 | 0 % |
| steady | 2 | 0 % |
| cylindrical | 2 | 0 % |
| strength | 2 | 0 % |
| pumps“ | 2 | 0 % |
| sumps | 2 | 0 % |
| variation | 2 | 0 % |
| rebound | 2 | 0 % |
| fft | 2 | 0 % |
| turbopumps | 2 | 0 % |
| atmospheric | 2 | 0 % |
| fuel | 2 | 0 % |
| photography | 2 | 0 % |
| review | 2 | 0 % |
| spark | 2 | 0 % |
| 1970 | 2 | 0 % |
| order | 2 | 0 % |
| vacuum | 2 | 0 % |
| single-phase | 2 | 0 % |
| achkinadze | 2 | 0 % |
| diagram | 2 | 0 % |
| cal | 2 | 0 % |
| condition.” | 2 | 0 % |
| joint-time | 2 | 0 % |
| diverson | 2 | 0 % |
| couty | 2 | 0 % |
| general | 2 | 0 % |
| maximum | 2 | 0 % |
| kunz | 2 | 0 % |
| bem | 2 | 0 % |
| tait | 2 | 0 % |
| hiroyasu | 2 | 0 % |
| spillway | 2 | 0 % |
| oxigen | 2 | 0 % |
| mapping | 2 | 0 % |
| third | 2 | 0 % |
| shear | 2 | 0 % |
| d | 2 | 0 % |
| geometrical | 2 | 0 % |
| tab_hty | 2 | 0 % |
| break | 2 | 0 % |
| “experimental | 2 | 0 % |
| applications | 2 | 0 % |
| modified | 2 | 0 % |
| foam | 2 | 0 % |
| 950080 | 2 | 0 % |
| specific | 2 | 0 % |
| section | 2 | 0 % |
| body | 2 | 0 % |
| internal | 2 | 0 % |
| separation | 2 | 0 % |
| pustoshny | 2 | 0 % |
| chahine | 2 | 0 % |
| cloud | 2 | 0 % |
| kaklinsky | 2 | 0 % |
| chimera | 2 | 0 % |
| iahr | 2 | 0 % |
| three | 2 | 0 % |
| lines | 2 | 0 % |
| transient | 2 | 0 % |
| short | 2 | 0 % |
| oriface | 2 | 0 % |
| university | 2 | 0 % |
| scaled | 2 | 0 % |
| .edu | 2 | 0 % |
| rouse | 2 | 0 % |
| steel | 2 | 0 % |
| viscous | 2 | 0 % |
| damping | 2 | 0 % |
| details | 2 | 0 % |
| properties | 2 | 0 % |
| machines | 2 | 0 % |
| conference | 2 | 0 % |
| screw | 2 | 0 % |
| supercavitation-problems | 2 | 0 % |
| integral | 2 | 0 % |
| shuji | 2 | 0 % |
| 2d-curved | 2 | 0 % |
| crash | 2 | 0 % |
| profile | 2 | 0 % |
| p. | 2 | 0 % |
| helium | 2 | 0 % |
| philippe | 2 | 0 % |
| vapor/gas | 2 | 0 % |
| gosman | 2 | 0 % |
| fission | 2 | 0 % |
| fluint | 2 | 0 % |
| proceeding | 2 | 0 % |
| explosive | 2 | 0 % |
| partial | 2 | 0 % |
| baghdassarian | 2 | 0 % |
| bearings | 2 | 0 % |
| a.d. | 2 | 0 % |
| via | 2 | 0 % |
| luminescence | 2 | 0 % |
| detecting | 2 | 0 % |
| phenomena | 2 | 0 % |
| micro | 2 | 0 % |
| condensation | 2 | 0 % |
| potential | 2 | 0 % |
| vol.8 | 2 | 0 % |
| sensor | 2 | 0 % |
| kinjo | 2 | 0 % |
| hydromechanics | 2 | 0 % |
| lattice | 2 | 0 % |
| becker | 2 | 0 % |
| level | 2 | 0 % |
| refrigerant | 2 | 0 % |
| simple | 2 | 0 % |
| entrainment | 2 | 0 % |
| circular | 2 | 0 % |
| sea | 2 | 0 % |
| site | 2 | 0 % |
| robert | 2 | 0 % |
| laboratory | 2 | 0 % |
| a.d.vasin | 2 | 0 % |
| dumont | 2 | 0 % |
| abstract | 2 | 0 % |
| kuklinski | 2 | 0 % |
| l/d | 2 | 0 % |
| meridional | 2 | 0 % |
| navsea | 2 | 0 % |
| neal | 2 | 0 % |
| studies | 2 | 0 % |
| epfl | 2 | 0 % |
| capuani | 2 | 0 % |
| tabbert | 2 | 0 % |
| hykat | 2 | 0 % |
| email | 1 | 0 % |
| storm | 1 | 0 % |
| nato/agaard | 1 | 0 % |
| particle | 1 | 0 % |
| serebryakov | 1 | 0 % |
| locating | 1 | 0 % |
| forming | 1 | 0 % |
| dimensioal | 1 | 0 % |
| stepanoff | 1 | 0 % |
| snaj | 1 | 0 % |
| nishida | 1 | 0 % |
| micro-bubble | 1 | 0 % |
| wall | 1 | 0 % |
| corotating | 1 | 0 % |
| direction | 1 | 0 % |
| accelerate | 1 | 0 % |
| developments | 1 | 0 % |
| panasonic | 1 | 0 % |
| lecroy | 1 | 0 % |
| knudsen | 1 | 0 % |
| explained | 1 | 0 % |
| yoshinobu | 1 | 0 % |
| coefficients | 1 | 0 % |
| dang | 1 | 0 % |
| subsonic | 1 | 0 % |
| hydrogen | 1 | 0 % |
| pump-comparison | 1 | 0 % |
| neighbourhood | 1 | 0 % |
| cause | 1 | 0 % |
| id | 1 | 0 % |
| leeds | 1 | 0 % |
| very | 1 | 0 % |
| setting | 1 | 0 % |
| vertical | 1 | 0 % |
| shin | 1 | 0 % |
| inch | 1 | 0 % |
| pp. | 1 | 0 % |
| egusquiza | 1 | 0 % |
| surfaces | 1 | 0 % |
| check | 1 | 0 % |
| proceedings | 1 | 0 % |
| sheets | 1 | 0 % |
| desing | 1 | 0 % |
| fem | 1 | 0 % |
| lezzi | 1 | 0 % |
| virginia | 1 | 0 % |
| grid | 1 | 0 % |
| mohamed | 1 | 0 % |
| produced | 1 | 0 % |
| precession | 1 | 0 % |
| 8 | 1 | 0 % |
| equations | 1 | 0 % |
| numbers | 1 | 0 % |
| cavity-flow | 1 | 0 % |
| tables | 1 | 0 % |
| grid-embedding | 1 | 0 % |
| schiff | 1 | 0 % |
| vapor | 1 | 0 % |
| explosion | 1 | 0 % |
| transsonic | 1 | 0 % |
| rnners | 1 | 0 % |
| density | 1 | 0 % |
| top | 1 | 0 % |
| v.i. | 1 | 0 % |
| //cav2001.library.caltech.edu/ | 1 | 0 % |
| source | 1 | 0 % |
| protection | 1 | 0 % |
| front | 1 | 0 % |
| empirical | 1 | 0 % |
| splitting | 1 | 0 % |
| wei | 1 | 0 % |
| tsujimoto | 1 | 0 % |
| shf | 1 | 0 % |
| peening | 1 | 0 % |
| judge | 1 | 0 % |
| meeting | 1 | 0 % |
| c.l. | 1 | 0 % |
| 1975. | 1 | 0 % |
| rupture | 1 | 0 % |
| near-wall | 1 | 0 % |
| china | 1 | 0 % |
| supersonic | 1 | 0 % |
| ignition | 1 | 0 % |
| 0012 | 1 | 0 % |
| acrylic-resin | 1 | 0 % |
| multi-hole | 1 | 0 % |
| 1 | 1 | 0 % |
| cf | 1 | 0 % |
| flat | 1 | 0 % |
| multihole | 1 | 0 % |
| contact | 1 | 0 % |
| 1973 | 1 | 0 % |
| lund | 1 | 0 % |
| turbin.pdf | 1 | 0 % |
| cavitatingflows | 1 | 0 % |
| naca0020 | 1 | 0 % |
| meyer | 1 | 0 % |
| p | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| georges | 1 | 0 % |
| tow-dimensional | 1 | 0 % |
| -springerlink | 1 | 0 % |
| dtmb | 1 | 0 % |
| fluctuations.pdf | 1 | 0 % |
| injectors | 1 | 0 % |
| f. | 1 | 0 % |
| soyama | 1 | 0 % |
| supply | 1 | 0 % |
| berndt | 1 | 0 % |
| e-mail | 1 | 0 % |
| roll-up | 1 | 0 % |
| poincare-lighthill-kuo | 1 | 0 % |
| analyzing | 1 | 0 % |
| numericals | 1 | 0 % |
| concave | 1 | 0 % |
| 1981 | 1 | 0 % |
| akamatsu | 1 | 0 % |
| g. | 1 | 0 % |
| patterning | 1 | 0 % |
| resonant | 1 | 0 % |
| oti | 1 | 0 % |
| two-phase | 1 | 0 % |
| precondition | 1 | 0 % |
| habchi | 1 | 0 % |
| similar | 1 | 0 % |
| prandtl | 1 | 0 % |
| p. | 1 | 0 % |
| doc | 1 | 0 % |
| fine/turbo | 1 | 0 % |
| acosta | 1 | 0 % |
| jacobians | 1 | 0 % |
| lovik | 1 | 0 % |
| d-amps | 1 | 0 % |
| unstable | 1 | 0 % |
| degassing | 1 | 0 % |
| azimutal | 1 | 0 % |
| virtue | 1 | 0 % |
| restricting | 1 | 0 % |
| extracorporeal | 1 | 0 % |
| 212 | 1 | 0 % |
| sassanelli | 1 | 0 % |
| make | 1 | 0 % |
| henschel | 1 | 0 % |
| non-spherical | 1 | 0 % |
| maitre | 1 | 0 % |
| coeff | 1 | 0 % |
| michel@caltech.edu | 1 | 0 % |
| ft/sec | 1 | 0 % |
| www.gidb.itu.edu.tr/staff | 1 | 0 % |
| runge | 1 | 0 % |
| utilization | 1 | 0 % |
| fürst | 1 | 0 % |
| impacts | 1 | 0 % |
| some | 1 | 0 % |
| pulse | 1 | 0 % |
| result | 1 | 0 % |
| recirculation | 1 | 0 % |
| naca66-12% | 1 | 0 % |
| vulcain | 1 | 0 % |
| motor | 1 | 0 % |
| advantages | 1 | 0 % |
| lcc | 1 | 0 % |
| coutier | 1 | 0 % |
| mist | 1 | 0 % |
| radiated | 1 | 0 % |
| constant | 1 | 0 % |
| techniques | 1 | 0 % |
| stripling | 1 | 0 % |
| -air | 1 | 0 % |
| against | 1 | 0 % |
| merkle | 1 | 0 % |
| capture | 1 | 0 % |
| or | 1 | 0 % |
| expression | 1 | 0 % |
| does | 1 | 0 % |
| geometrically | 1 | 0 % |
| mitsui | 1 | 0 % |
| b.r. | 1 | 0 % |
| research | 1 | 0 % |
| solutions | 1 | 0 % |
| simonin | 1 | 0 % |
| . | 1 | 0 % |
| improve | 1 | 0 % |
| naca0012 | 1 | 0 % |
| space | 1 | 0 % |
| heating | 1 | 0 % |
| parts | 1 | 0 % |
| incubation | 1 | 0 % |
| silicone | 1 | 0 % |
| statistics | 1 | 0 % |
| 102 | 1 | 0 % |
| program | 1 | 0 % |
| microscale | 1 | 0 % |
| 006 | 1 | 0 % |
| power | 1 | 0 % |
| elastic | 1 | 0 % |
| e | 1 | 0 % |
| discuss | 1 | 0 % |
| watt | 1 | 0 % |
| .69 | 1 | 0 % |
| period | 1 | 0 % |
| pump.pdf | 1 | 0 % |
| y. | 1 | 0 % |
| refrence | 1 | 0 % |
| delta | 1 | 0 % |
| orifice.pdf | 1 | 0 % |
| e. | 1 | 0 % |
| flashing | 1 | 0 % |
| sigma | 1 | 0 % |
| operating | 1 | 0 % |
| british | 1 | 0 % |
| velocities | 1 | 0 % |
| und | 1 | 0 % |
| 1999-01-0524 | 1 | 0 % |
| hybrid | 1 | 0 % |
| thought | 1 | 0 % |
| rodi | 1 | 0 % |
| kalumuck | 1 | 0 % |
| yu. | 1 | 0 % |
| piv | 1 | 0 % |
| two-dimensional | 1 | 0 % |
| 10-inch | 1 | 0 % |
| ratios | 1 | 0 % |
| hara | 1 | 0 % |
| stoffel@tfa.tu-darmstadt.de | 1 | 0 % |
| vladimir.n.semenenko | 1 | 0 % |
| low-reynolds-number | 1 | 0 % |
| shedding | 1 | 0 % |
| doe | 1 | 0 % |
| cavtataion | 1 | 0 % |
| kulite | 1 | 0 % |
| including | 1 | 0 % |
| x-ray | 1 | 0 % |
| sciences | 1 | 0 % |
| ashwin | 1 | 0 % |
| cavatating | 1 | 0 % |
| why | 1 | 0 % |
| mit | 1 | 0 % |
| interferometry | 1 | 0 % |
| know | 1 | 0 % |
| manual | 1 | 0 % |
| content | 1 | 0 % |
| equivalence | 1 | 0 % |
| hypervelocity | 1 | 0 % |
| course | 1 | 0 % |
| hub | 1 | 0 % |
| turbin | 1 | 0 % |
| engineer | 1 | 0 % |
| lower | 1 | 0 % |
| negative | 1 | 0 % |
| honeycomb | 1 | 0 % |
| fortran | 1 | 0 % |
| centerd | 1 | 0 % |
| kvaerner | 1 | 0 % |
| kidney | 1 | 0 % |
| erosional | 1 | 0 % |
| dans | 1 | 0 % |
| 474 | 1 | 0 % |
| quasi-one-dimensional | 1 | 0 % |
| sections | 1 | 0 % |
| edges | 1 | 0 % |
| m. | 1 | 0 % |
| continuity | 1 | 0 % |
| leo | 1 | 0 % |
| bottom | 1 | 0 % |
| multiple | 1 | 0 % |
| maneuver | 1 | 0 % |
| shaped | 1 | 0 % |
| characterstics | 1 | 0 % |
| hot | 1 | 0 % |
| thermo-fluid | 1 | 0 % |
| etude | 1 | 0 % |
| wingtip | 1 | 0 % |
| orthogonal | 1 | 0 % |
| pdf.com | 1 | 0 % |
| et | 1 | 0 % |
| louis | 1 | 0 % |
| o. | 1 | 0 % |
| reynolds-averaged | 1 | 0 % |
| resolution | 1 | 0 % |
| d. | 1 | 0 % |
| vedio | 1 | 0 % |
| xtm | 1 | 0 % |
| tot | 1 | 0 % |
| albunex | 1 | 0 % |
| newton | 1 | 0 % |
| j. | 1 | 0 % |
| recommended | 1 | 0 % |
| n | 1 | 0 % |
| upper | 1 | 0 % |
| bulbous | 1 | 0 % |
| wake-field | 1 | 0 % |
| cavİtatİon | 1 | 0 % |
| 44-53 | 1 | 0 % |
| environment | 1 | 0 % |
| wallis | 1 | 0 % |
| delale | 1 | 0 % |
| ido | 1 | 0 % |
| kutta | 1 | 0 % |
| late | 1 | 0 % |
| generator | 1 | 0 % |
| g | 1 | 0 % |
| derivation | 1 | 0 % |
| medwin | 1 | 0 % |
| open | 1 | 0 % |
| rader | 1 | 0 % |
| yuka | 1 | 0 % |
| retaliating | 1 | 0 % |
| area | 1 | 0 % |
| p.p | 1 | 0 % |
| bubbles. | 1 | 0 % |
| propellrar | 1 | 0 % |
| nano | 1 | 0 % |
| transform | 1 | 0 % |
| jean-pierre | 1 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 1 | 0 % |
| plume | 1 | 0 % |
| radial | 1 | 0 % |
| latent | 1 | 0 % |
| probing | 1 | 0 % |
| toe | 1 | 0 % |
| lu | 1 | 0 % |
| scheuerer | 1 | 0 % |
| a.j. | 1 | 0 % |
| predict | 1 | 0 % |
| yuan | 1 | 0 % |
| detachment | 1 | 0 % |
| swales | 1 | 0 % |
| eno | 1 | 0 % |
| commercial | 1 | 0 % |
| stinebring | 1 | 0 % |
| sprays | 1 | 0 % |
| 1986 | 1 | 0 % |
| 40k | 1 | 0 % |
| efect | 1 | 0 % |
| instabilities | 1 | 0 % |
| dam | 1 | 0 % |
| narayana | 1 | 0 % |
| 1917. | 1 | 0 % |
| holes | 1 | 0 % |
| Other words | 504 | 8.3 % |
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