| 1357 different keywords | Search | Percent |
|---|
| cavitation | 516 | 9.1 % |
| pdf | 161 | 2.8 % |
| of | 149 | 2.6 % |
| propeller | 146 | 2.5 % |
| in | 78 | 1.3 % |
| pump | 77 | 1.3 % |
| vortex | 70 | 1.2 % |
| and | 63 | 1.1 % |
| supercavitation | 60 | 1 % |
| flow | 54 | 0.9 % |
| orifice | 51 | 0.9 % |
| centrifugal | 50 | 0.8 % |
| filetype | 48 | 0.8 % |
| fluent | 46 | 0.8 % |
| bubble | 44 | 0.7 % |
| ship | 43 | 0.7 % |
| pressure | 40 | 0.7 % |
| surface | 39 | 0.6 % |
| the | 38 | 0.6 % |
| on | 37 | 0.6 % |
| pumps | 36 | 0.6 % |
| supercavitating | 35 | 0.6 % |
| cavity | 33 | 0.5 % |
| model | 32 | 0.5 % |
| restriction | 32 | 0.5 % |
| cavitating | 32 | 0.5 % |
| water | 31 | 0.5 % |
| a | 29 | 0.5 % |
| bubbles | 29 | 0.5 % |
| blade | 29 | 0.5 % |
| propellers | 28 | 0.4 % |
| piercing | 27 | 0.4 % |
| analysis | 25 | 0.4 % |
| nozzle | 25 | 0.4 % |
| equation | 24 | 0.4 % |
| for | 24 | 0.4 % |
| number | 23 | 0.4 % |
| hydrofoil | 23 | 0.4 % |
| cfd | 22 | 0.3 % |
| turbine | 21 | 0.3 % |
| time | 21 | 0.3 % |
| rudder | 21 | 0.3 % |
| numerical | 20 | 0.3 % |
| tip | 20 | 0.3 % |
| method | 20 | 0.3 % |
| frequency | 20 | 0.3 % |
| symposium | 19 | 0.3 % |
| jet | 19 | 0.3 % |
| cav2001 | 19 | 0.3 % |
| design | 19 | 0.3 % |
| diesel | 19 | 0.3 % |
| noise | 19 | 0.3 % |
| effect | 18 | 0.3 % |
| dynamics | 17 | 0.3 % |
| how | 17 | 0.3 % |
| inducer | 17 | 0.3 % |
| joint | 17 | 0.3 % |
| calculation | 17 | 0.3 % |
| inception | 17 | 0.3 % |
| erosion | 16 | 0.2 % |
| impeller | 16 | 0.2 % |
| international | 16 | 0.2 % |
| kaplan | 16 | 0.2 % |
| intake | 15 | 0.2 % |
| speed | 15 | 0.2 % |
| azipod | 14 | 0.2 % |
| tunnel | 14 | 0.2 % |
| submerged | 14 | 0.2 % |
| naca | 13 | 0.2 % |
| simulation | 13 | 0.2 % |
| fluid | 12 | 0.2 % |
| distribution | 12 | 0.2 % |
| to | 12 | 0.2 % |
| modeling | 12 | 0.2 % |
| orifices | 12 | 0.2 % |
| micro | 12 | 0.2 % |
| nexearch | 12 | 0.2 % |
| video | 11 | 0.1 % |
| hull | 11 | 0.1 % |
| flows | 11 | 0.1 % |
| webkr | 11 | 0.1 % |
| velocity | 11 | 0.1 % |
| angle | 11 | 0.1 % |
| types | 11 | 0.1 % |
| suction | 11 | 0.1 % |
| experimental | 11 | 0.1 % |
| turbopump | 10 | 0.1 % |
| 2001 | 10 | 0.1 % |
| savchenko | 10 | 0.1 % |
| coefficient | 10 | 0.1 % |
| cavitator | 10 | 0.1 % |
| damage | 10 | 0.1 % |
| .pdf | 10 | 0.1 % |
| jets | 9 | 0.1 % |
| super | 9 | 0.1 % |
| experiment | 9 | 0.1 % |
| study | 9 | 0.1 % |
| injector | 9 | 0.1 % |
| test | 9 | 0.1 % |
| acoustic | 9 | 0.1 % |
| boundary | 9 | 0.1 % |
| are | 9 | 0.1 % |
| npsh | 9 | 0.1 % |
| valve | 9 | 0.1 % |
| supercavity | 9 | 0.1 % |
| effects | 9 | 0.1 % |
| bodies | 8 | 0.1 % |
| unsteady | 8 | 0.1 % |
| & | 8 | 0.1 % |
| liquid | 8 | 0.1 % |
| sump | 8 | 0.1 % |
| paper | 8 | 0.1 % |
| stokes | 8 | 0.1 % |
| ventilated | 8 | 0.1 % |
| thesis | 8 | 0.1 % |
| vibration | 8 | 0.1 % |
| two | 8 | 0.1 % |
| cav | 8 | 0.1 % |
| rotor | 8 | 0.1 % |
| particle | 7 | 0.1 % |
| drag | 7 | 0.1 % |
| pipe | 7 | 0.1 % |
| performance | 7 | 0.1 % |
| injectors | 7 | 0.1 % |
| index | 7 | 0.1 % |
| turbines | 7 | 0.1 % |
| time-frequency | 7 | 0.1 % |
| theory | 7 | 0.1 % |
| compressible | 7 | 0.1 % |
| edge | 7 | 0.1 % |
| geometry | 7 | 0.1 % |
| problems | 7 | 0.1 % |
| cloud | 7 | 0.1 % |
| clearance | 7 | 0.1 % |
| gas | 7 | 0.1 % |
| hydraulic | 7 | 0.1 % |
| closure | 6 | 0.1 % |
| projectile | 6 | 0.1 % |
| measurement | 6 | 0.1 % |
| underwater | 6 | 0.1 % |
| inlet | 6 | 0.1 % |
| mass | 6 | 0.1 % |
| b. | 6 | 0.1 % |
| rayleigh-plesset | 6 | 0.1 % |
| axial | 6 | 0.1 % |
| foil | 6 | 0.1 % |
| atlar | 6 | 0.1 % |
| 3d | 6 | 0.1 % |
| stability | 6 | 0.1 % |
| plate | 6 | 0.1 % |
| diagram | 6 | 0.1 % |
| m. | 6 | 0.1 % |
| stoffel | 6 | 0.1 % |
| sato | 6 | 0.1 % |
| generator | 6 | 0.1 % |
| sheet | 6 | 0.1 % |
| modelling | 6 | 0.1 % |
| instabilities | 6 | 0.1 % |
| ships | 6 | 0.1 % |
| horn | 5 | 0 % |
| by | 5 | 0 % |
| naca0015 | 5 | 0 % |
| journal | 5 | 0 % |
| about | 5 | 0 % |
| ring | 5 | 0 % |
| collapse | 5 | 0 % |
| oscillation | 5 | 0 % |
| formed | 5 | 0 % |
| naca66 | 5 | 0 % |
| formula | 5 | 0 % |
| fine | 5 | 0 % |
| sound | 5 | 0 % |
| introduction | 5 | 0 % |
| panel | 5 | 0 % |
| hydrodynamic | 5 | 0 % |
| low | 5 | 0 % |
| molecular | 5 | 0 % |
| with | 5 | 0 % |
| bearing | 5 | 0 % |
| propulsion | 5 | 0 % |
| wake | 5 | 0 % |
| numeca | 5 | 0 % |
| tank | 5 | 0 % |
| injection | 5 | 0 % |
| data | 5 | 0 % |
| kudo | 5 | 0 % |
| span | 5 | 0 % |
| wave | 5 | 0 % |
| venturi | 5 | 0 % |
| turbulence | 5 | 0 % |
| viscous | 5 | 0 % |
| hoffmann | 5 | 0 % |
| turbo | 5 | 0 % |
| waterjet | 5 | 0 % |
| 2d | 5 | 0 % |
| spectrum | 5 | 0 % |
| lee | 5 | 0 % |
| kuklinski | 5 | 0 % |
| what | 4 | 0 % |
| wall | 4 | 0 % |
| incipient | 4 | 0 % |
| yuriy | 4 | 0 % |
| froude | 4 | 0 % |
| helical | 4 | 0 % |
| heat | 4 | 0 % |
| equations | 4 | 0 % |
| perspectives | 4 | 0 % |
| steering | 4 | 0 % |
| piping | 4 | 0 % |
| dependent | 4 | 0 % |
| institute | 4 | 0 % |
| instability | 4 | 0 % |
| state | 4 | 0 % |
| naca0020 | 4 | 0 % |
| reentrant | 4 | 0 % |
| cone | 4 | 0 % |
| butterfly | 4 | 0 % |
| hydrofoils | 4 | 0 % |
| parameters | 4 | 0 % |
| rotating | 4 | 0 % |
| aisi | 4 | 0 % |
| free | 4 | 0 % |
| some | 4 | 0 % |
| measurements | 4 | 0 % |
| channel | 4 | 0 % |
| rocket | 4 | 0 % |
| large | 4 | 0 % |
| location | 4 | 0 % |
| reynolds | 4 | 0 % |
| shape | 4 | 0 % |
| interaction | 4 | 0 % |
| inside | 4 | 0 % |
| pictures | 4 | 0 % |
| strouhal | 4 | 0 % |
| code | 4 | 0 % |
| history | 4 | 0 % |
| turbulent | 4 | 0 % |
| - | 4 | 0 % |
| les | 4 | 0 % |
| coupling | 4 | 0 % |
| mine | 4 | 0 % |
| mechanism | 4 | 0 % |
| 5 | 4 | 0 % |
| entry | 4 | 0 % |
| ultrasound | 4 | 0 % |
| specific | 4 | 0 % |
| section | 4 | 0 % |
| characteristics | 4 | 0 % |
| spray | 4 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 4 | 0 % |
| using | 4 | 0 % |
| singularity | 4 | 0 % |
| cavities | 4 | 0 % |
| lubrication | 4 | 0 % |
| plume | 4 | 0 % |
| navier | 4 | 0 % |
| mixed | 4 | 0 % |
| induced | 4 | 0 % |
| luminescence | 4 | 0 % |
| plesset | 4 | 0 % |
| characteristic | 4 | 0 % |
| site | 4 | 0 % |
| robert | 4 | 0 % |
| 1055 | 4 | 0 % |
| near | 4 | 0 % |
| hammer | 4 | 0 % |
| neal | 4 | 0 % |
| rayleigh | 4 | 0 % |
| at | 4 | 0 % |
| f | 4 | 0 % |
| sonoluminescence | 4 | 0 % |
| n. | 3 | 0 % |
| finite | 3 | 0 % |
| rotation | 3 | 0 % |
| shapes | 3 | 0 % |
| energy | 3 | 0 % |
| maccormack | 3 | 0 % |
| phase | 3 | 0 % |
| 4th | 3 | 0 % |
| part | 3 | 0 % |
| sauer | 3 | 0 % |
| viscosity | 3 | 0 % |
| different | 3 | 0 % |
| vertical | 3 | 0 % |
| understanding | 3 | 0 % |
| caltech | 3 | 0 % |
| vortices | 3 | 0 % |
| transducer | 3 | 0 % |
| rate | 3 | 0 % |
| kotaro | 3 | 0 % |
| measuring | 3 | 0 % |
| step | 3 | 0 % |
| skew | 3 | 0 % |
| wing | 3 | 0 % |
| up | 3 | 0 % |
| speeds | 3 | 0 % |
| thermal | 3 | 0 % |
| kerwin | 3 | 0 % |
| nonlinear | 3 | 0 % |
| lecture | 3 | 0 % |
| oscillating | 3 | 0 % |
| impact | 3 | 0 % |
| evolution | 3 | 0 % |
| based | 3 | 0 % |
| gotfred | 3 | 0 % |
| added | 3 | 0 % |
| a8 | 3 | 0 % |
| solution | 3 | 0 % |
| transfer | 3 | 0 % |
| berntsen | 3 | 0 % |
| hydro | 3 | 0 % |
| an | 3 | 0 % |
| der | 3 | 0 % |
| acceleration | 3 | 0 % |
| interface | 3 | 0 % |
| turbomachinery | 3 | 0 % |
| propeler | 3 | 0 % |
| disk | 3 | 0 % |
| research | 3 | 0 % |
| naca4412 | 3 | 0 % |
| between | 3 | 0 % |
| vs | 3 | 0 % |
| power | 3 | 0 % |
| waves | 3 | 0 % |
| ando | 3 | 0 % |
| und | 3 | 0 % |
| formed? | 3 | 0 % |
| yu. | 3 | 0 % |
| multiphase | 3 | 0 % |
| total | 3 | 0 % |
| bem | 3 | 0 % |
| discharge | 3 | 0 % |
| axisymmetric | 3 | 0 % |
| engineering | 3 | 0 % |
| element | 3 | 0 % |
| transport | 3 | 0 % |
| shock | 3 | 0 % |
| size | 3 | 0 % |
| body | 3 | 0 % |
| hole | 3 | 0 % |
| single | 3 | 0 % |
| meter | 3 | 0 % |
| approach | 3 | 0 % |
| critical | 3 | 0 % |
| gap | 3 | 0 % |
| compressibility | 3 | 0 % |
| semenenko | 3 | 0 % |
| downstream | 3 | 0 % |
| transient | 3 | 0 % |
| npshr | 3 | 0 % |
| francis | 3 | 0 % |
| vapour | 3 | 0 % |
| tests | 3 | 0 % |
| airfoil | 3 | 0 % |
| temperature | 3 | 0 % |
| nicolas | 3 | 0 % |
| schnerr | 3 | 0 % |
| crash | 3 | 0 % |
| predict | 3 | 0 % |
| thrust | 3 | 0 % |
| xml_no_dtd | 3 | 0 % |
| partial | 3 | 0 % |
| processing | 3 | 0 % |
| watanabe | 3 | 0 % |
| hsva | 3 | 0 % |
| condition | 3 | 0 % |
| machinery | 3 | 0 % |
| cavitations | 3 | 0 % |
| keller | 3 | 0 % |
| region | 3 | 0 % |
| drop | 3 | 0 % |
| from | 3 | 0 % |
| kjeldsen | 3 | 0 % |
| 66 | 3 | 0 % |
| morten | 3 | 0 % |
| schmidt | 3 | 0 % |
| lifting | 3 | 0 % |
| high-speed | 3 | 0 % |
| leading | 3 | 0 % |
| dumont | 3 | 0 % |
| photos | 3 | 0 % |
| high | 3 | 0 % |
| stop | 3 | 0 % |
| leakage | 3 | 0 % |
| industries | 3 | 0 % |
| air | 3 | 0 % |
| caviation | 2 | 0 % |
| trans | 2 | 0 % |
| martin | 2 | 0 % |
| used | 2 | 0 % |
| equilibrium | 2 | 0 % |
| steps | 2 | 0 % |
| figure | 2 | 0 % |
| system | 2 | 0 % |
| author | 2 | 0 % |
| i-senocak | 2 | 0 % |
| procedure | 2 | 0 % |
| ikohagi | 2 | 0 % |
| sv | 2 | 0 % |
| schaffar | 2 | 0 % |
| explained | 2 | 0 % |
| can | 2 | 0 % |
| yoshinobu | 2 | 0 % |
| yoshiki | 2 | 0 % |
| hardness | 2 | 0 % |
| national | 2 | 0 % |
| screws | 2 | 0 % |
| self-oscillating | 2 | 0 % |
| plates | 2 | 0 % |
| nuclation | 2 | 0 % |
| computational | 2 | 0 % |
| type | 2 | 0 % |
| runner | 2 | 0 % |
| problem | 2 | 0 % |
| structural | 2 | 0 % |
| solid | 2 | 0 % |
| laminar | 2 | 0 % |
| analyses | 2 | 0 % |
| gopalan | 2 | 0 % |
| kevin | 2 | 0 % |
| kam | 2 | 0 % |
| density | 2 | 0 % |
| joussellin | 2 | 0 % |
| identify | 2 | 0 % |
| tsujimoto | 2 | 0 % |
| spectra | 2 | 0 % |
| vickers | 2 | 0 % |
| compressor | 2 | 0 % |
| laser | 2 | 0 % |
| supersonic | 2 | 0 % |
| facing | 2 | 0 % |
| axis | 2 | 0 % |
| artificial | 2 | 0 % |
| j | 2 | 0 % |
| fluctuations | 2 | 0 % |
| ali | 2 | 0 % |
| bell | 2 | 0 % |
| pd | 2 | 0 % |
| scale | 2 | 0 % |
| chart | 2 | 0 % |
| flapped | 2 | 0 % |
| sname | 2 | 0 % |
| vof | 2 | 0 % |
| pumping | 2 | 0 % |
| emission | 2 | 0 % |
| compounds | 2 | 0 % |
| von | 2 | 0 % |
| georges | 2 | 0 % |
| hsieh | 2 | 0 % |
| super-cavitation | 2 | 0 % |
| regiane | 2 | 0 % |
| over | 2 | 0 % |
| visualization | 2 | 0 % |
| is | 2 | 0 % |
| pipes | 2 | 0 % |
| oxidize | 2 | 0 % |
| naval | 2 | 0 % |
| cascade | 2 | 0 % |
| ng | 2 | 0 % |
| yoshida | 2 | 0 % |
| bladed | 2 | 0 % |
| oberflache | 2 | 0 % |
| curvilinear | 2 | 0 % |
| gleitvarangange | 2 | 0 % |
| flash | 2 | 0 % |
| acosta | 2 | 0 % |
| valves | 2 | 0 % |
| ventilation | 2 | 0 % |
| skewed | 2 | 0 % |
| torpedo | 2 | 0 % |
| jessup | 2 | 0 % |
| through | 2 | 0 % |
| fluctuation | 2 | 0 % |
| 7 | 2 | 0 % |
| triangle | 2 | 0 % |
| eulerian-lagrangian | 2 | 0 % |
| undersea | 2 | 0 % |
| line | 2 | 0 % |
| similarity | 2 | 0 % |
| surge | 2 | 0 % |
| layer | 2 | 0 % |
| sae | 2 | 0 % |
| spectrometer | 2 | 0 % |
| uber | 2 | 0 % |
| generalized | 2 | 0 % |
| motion | 2 | 0 % |
| set | 2 | 0 % |
| destroyers | 2 | 0 % |
| camera | 2 | 0 % |
| stripling | 2 | 0 % |
| lithotripsy | 2 | 0 % |
| ocean | 2 | 0 % |
| investigations | 2 | 0 % |
| or | 2 | 0 % |
| organic | 2 | 0 % |
| slant | 2 | 0 % |
| kinnas | 2 | 0 % |
| pod | 2 | 0 % |
| dhiman | 2 | 0 % |
| fortes-patella | 2 | 0 % |
| thornycroft | 2 | 0 % |
| implement | 2 | 0 % |
| inviscid | 2 | 0 % |
| wavelet | 2 | 0 % |
| force | 2 | 0 % |
| heating | 2 | 0 % |
| experiments | 2 | 0 % |
| motions | 2 | 0 % |
| heavy | 2 | 0 % |
| re-entrant | 2 | 0 % |
| reduction | 2 | 0 % |
| platzer | 2 | 0 % |
| v.n. | 2 | 0 % |
| attack | 2 | 0 % |
| strength | 2 | 0 % |
| nozzles | 2 | 0 % |
| turbopumps | 2 | 0 % |
| narrow | 2 | 0 % |
| systems | 2 | 0 % |
| gp-mf | 2 | 0 % |
| chatterjee | 2 | 0 % |
| values | 2 | 0 % |
| capturing | 2 | 0 % |
| senocak | 2 | 0 % |
| shedding | 2 | 0 % |
| barnaby | 2 | 0 % |
| erosive | 2 | 0 % |
| control | 2 | 0 % |
| back | 2 | 0 % |
| cp | 2 | 0 % |
| tait | 2 | 0 % |
| pattern | 2 | 0 % |
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| content | 2 | 0 % |
| d | 2 | 0 % |
| string | 2 | 0 % |
| hypervelocity | 2 | 0 % |
| tensile | 2 | 0 % |
| behaviour | 2 | 0 % |
| turbin | 2 | 0 % |
| scheme | 2 | 0 % |
| 1997 | 2 | 0 % |
| shridhar | 2 | 0 % |
| hosangadi | 2 | 0 % |
| cryogenic | 2 | 0 % |
| thoma | 2 | 0 % |
| signal | 2 | 0 % |
| chahine | 2 | 0 % |
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| circuit | 2 | 0 % |
| logvinovich | 2 | 0 % |
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| area | 2 | 0 % |
| technique | 2 | 0 % |
| supercavitation-problems | 2 | 0 % |
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| height | 2 | 0 % |
| correction | 2 | 0 % |
| p. | 2 | 0 % |
| flussigkaiten | 2 | 0 % |
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| testing | 2 | 0 % |
| sonochemistry | 2 | 0 % |
| potential | 2 | 0 % |
| dimotakis | 2 | 0 % |
| cav2001.library.caltech.edu/126/00/cav2001_hofmann.pdf | 2 | 0 % |
| mixing | 2 | 0 % |
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| efficiency | 2 | 0 % |
| installation | 2 | 0 % |
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| 1999-01-1486 | 2 | 0 % |
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| calculate | 2 | 0 % |
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| preconditioning | 2 | 0 % |
| gabor | 2 | 0 % |
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| stopping | 1 | 0 % |
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| lie | 1 | 0 % |
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| co. | 1 | 0 % |
| nasa | 1 | 0 % |
| munition | 1 | 0 % |
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| correlation | 1 | 0 % |
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| sweep | 1 | 0 % |
| naca-0020 | 1 | 0 % |
| industrial | 1 | 0 % |
| mechanics | 1 | 0 % |
| smith | 1 | 0 % |
| means | 1 | 0 % |
| m/s | 1 | 0 % |
| npl | 1 | 0 % |
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| requirements | 1 | 0 % |
| 8 | 1 | 0 % |
| naca66mod | 1 | 0 % |
| inection | 1 | 0 % |
| bulbs | 1 | 0 % |
| tables | 1 | 0 % |
| race | 1 | 0 % |
| 103a02 | 1 | 0 % |
| vapor | 1 | 0 % |
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| weber | 1 | 0 % |
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| empirical | 1 | 0 % |
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| horn-type | 1 | 0 % |
| into | 1 | 0 % |
| time-dependent | 1 | 0 % |
| pda50 | 1 | 0 % |
| ratio | 1 | 0 % |
| solved | 1 | 0 % |
| jae-moon | 1 | 0 % |
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| wall-function | 1 | 0 % |
| www.howstuffworks.com | 1 | 0 % |
| max | 1 | 0 % |
| roll | 1 | 0 % |
| 0012 | 1 | 0 % |
| express | 1 | 0 % |
| 1 | 1 | 0 % |
| drift | 1 | 0 % |
| john | 1 | 0 % |
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| reverse | 1 | 0 % |
| liquids | 1 | 0 % |
| allmaras | 1 | 0 % |
| finish | 1 | 0 % |
| workshop | 1 | 0 % |
| mehmet | 1 | 0 % |
| lund | 1 | 0 % |
| he | 1 | 0 % |
| prausnitz | 1 | 0 % |
| behavior | 1 | 0 % |
| p | 1 | 0 % |
| facilities | 1 | 0 % |
| predictor-corrector | 1 | 0 % |
| gabrielli | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| bar | 1 | 0 % |
| wetted | 1 | 0 % |
| s.and | 1 | 0 % |
| horizontal | 1 | 0 % |
| navier–stokes | 1 | 0 % |
| 1993 | 1 | 0 % |
| pcb309a | 1 | 0 % |
| cavitastion | 1 | 0 % |
| lubricant | 1 | 0 % |
| mccormick | 1 | 0 % |
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| Ｒａｙｌｅｉｇｈ－Ｐｌｅｓｓｅｔ Ｅｑｕａｔｉｏｎ | 1 | 0 % |
| caita | 1 | 0 % |
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| ” | 1 | 0 % |
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| //journals.cambridge.org/article_s0022112000002925 | 1 | 0 % |
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| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx; | 1 | 0 % |
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| provider=microsoft.jet.oledb.4.0 | 1 | 0 % |
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| Other words | 358 | 6.3 % |