| 1421 different keywords | Search | Percent |
|---|
| cavitation | 545 | 8.3 % |
| of | 198 | 3 % |
| pdf | 177 | 2.7 % |
| propeller | 131 | 1.9 % |
| pump | 125 | 1.9 % |
| in | 108 | 1.6 % |
| orifice | 94 | 1.4 % |
| and | 70 | 1 % |
| bubble | 68 | 1 % |
| vortex | 66 | 1 % |
| the | 64 | 0.9 % |
| centrifugal | 63 | 0.9 % |
| for | 62 | 0.9 % |
| flow | 58 | 0.8 % |
| filetype | 58 | 0.8 % |
| restriction | 57 | 0.8 % |
| a | 54 | 0.8 % |
| fluent | 54 | 0.8 % |
| on | 47 | 0.7 % |
| bubbles | 44 | 0.6 % |
| numerical | 42 | 0.6 % |
| pressure | 41 | 0.6 % |
| boundary | 39 | 0.5 % |
| water | 37 | 0.5 % |
| model | 36 | 0.5 % |
| analysis | 36 | 0.5 % |
| element | 32 | 0.4 % |
| pumps | 32 | 0.4 % |
| effect | 31 | 0.4 % |
| cavitating | 28 | 0.4 % |
| simulation | 28 | 0.4 % |
| supercavitation | 27 | 0.4 % |
| propellers | 27 | 0.4 % |
| ship | 27 | 0.4 % |
| cavity | 26 | 0.3 % |
| equation | 26 | 0.3 % |
| to | 25 | 0.3 % |
| surface | 24 | 0.3 % |
| hydrofoil | 24 | 0.3 % |
| supercavitating | 24 | 0.3 % |
| jet | 23 | 0.3 % |
| inducer | 22 | 0.3 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 22 | 0.3 % |
| method | 22 | 0.3 % |
| kaplan | 22 | 0.3 % |
| introduction | 21 | 0.3 % |
| turbine | 21 | 0.3 % |
| suction | 21 | 0.3 % |
| nozzle | 21 | 0.3 % |
| collapse | 20 | 0.3 % |
| liquid | 20 | 0.3 % |
| tip | 20 | 0.3 % |
| design | 20 | 0.3 % |
| blade | 19 | 0.2 % |
| plesset | 19 | 0.2 % |
| piercing | 19 | 0.2 % |
| noise | 19 | 0.2 % |
| number | 18 | 0.2 % |
| erosion | 18 | 0.2 % |
| diesel | 18 | 0.2 % |
| sheet | 18 | 0.2 % |
| orifices | 18 | 0.2 % |
| tunnel | 17 | 0.2 % |
| experimental | 17 | 0.2 % |
| azipod | 16 | 0.2 % |
| types | 16 | 0.2 % |
| speed | 16 | 0.2 % |
| joint | 16 | 0.2 % |
| rayleigh | 16 | 0.2 % |
| nexearch | 16 | 0.2 % |
| unsteady | 15 | 0.2 % |
| hydrodynamic | 15 | 0.2 % |
| tab_hty | 15 | 0.2 % |
| modelling | 15 | 0.2 % |
| inception | 15 | 0.2 % |
| performance | 14 | 0.2 % |
| re-entrant | 14 | 0.2 % |
| time | 14 | 0.2 % |
| abstract | 14 | 0.2 % |
| dynamics | 13 | 0.1 % |
| laser | 13 | 0.1 % |
| naca | 13 | 0.1 % |
| plate | 13 | 0.1 % |
| spectrum | 13 | 0.1 % |
| phase | 12 | 0.1 % |
| 1 | 12 | 0.1 % |
| paper | 12 | 0.1 % |
| cav2001 | 12 | 0.1 % |
| modeling | 12 | 0.1 % |
| cfd | 12 | 0.1 % |
| calculation | 12 | 0.1 % |
| high | 12 | 0.1 % |
| experiment | 11 | 0.1 % |
| symposium | 11 | 0.1 % |
| how | 11 | 0.1 % |
| is | 11 | 0.1 % |
| acoustic | 11 | 0.1 % |
| hydrofoils | 11 | 0.1 % |
| velocity | 11 | 0.1 % |
| an | 11 | 0.1 % |
| hole | 11 | 0.1 % |
| what | 10 | 0.1 % |
| video | 10 | 0.1 % |
| intake | 10 | 0.1 % |
| test | 10 | 0.1 % |
| cavitator | 10 | 0.1 % |
| time-frequency | 10 | 0.1 % |
| angle | 10 | 0.1 % |
| lithotripsy | 10 | 0.1 % |
| multiphase | 10 | 0.1 % |
| two-dimensional | 10 | 0.1 % |
| impeller | 10 | 0.1 % |
| spherical | 10 | 0.1 % |
| international | 10 | 0.1 % |
| shock | 10 | 0.1 % |
| during | 10 | 0.1 % |
| two | 10 | 0.1 % |
| integral | 10 | 0.1 % |
| 2d | 10 | 0.1 % |
| frequency | 10 | 0.1 % |
| rudder | 10 | 0.1 % |
| underwater | 9 | 0.1 % |
| fluid | 9 | 0.1 % |
| partially | 9 | 0.1 % |
| distribution | 9 | 0.1 % |
| flows | 9 | 0.1 % |
| asme | 9 | 0.1 % |
| with | 9 | 0.1 % |
| solution | 9 | 0.1 % |
| damage | 9 | 0.1 % |
| core | 9 | 0.1 % |
| cryogenic | 9 | 0.1 % |
| ships | 9 | 0.1 % |
| from | 9 | 0.1 % |
| by | 8 | 0.1 % |
| pipe | 8 | 0.1 % |
| rayleigh-plesset | 8 | 0.1 % |
| & | 8 | 0.1 % |
| panel | 8 | 0.1 % |
| developed | 8 | 0.1 % |
| edge | 8 | 0.1 % |
| history | 8 | 0.1 % |
| tank | 8 | 0.1 % |
| turbin | 8 | 0.1 % |
| prediction | 8 | 0.1 % |
| head | 8 | 0.1 % |
| at | 8 | 0.1 % |
| closure | 7 | 0.1 % |
| equations | 7 | 0.1 % |
| journal | 7 | 0.1 % |
| mass | 7 | 0.1 % |
| coefficient | 7 | 0.1 % |
| stokes | 7 | 0.1 % |
| rotating | 7 | 0.1 % |
| foil | 7 | 0.1 % |
| turbomachinery | 7 | 0.1 % |
| between | 7 | 0.1 % |
| les | 7 | 0.1 % |
| wave | 7 | 0.1 % |
| methods | 7 | 0.1 % |
| .pdf | 7 | 0.1 % |
| dynamic | 7 | 0.1 % |
| submarine | 7 | 0.1 % |
| luminescence | 7 | 0.1 % |
| hydraulic | 7 | 0.1 % |
| robert | 7 | 0.1 % |
| kuklinski | 7 | 0.1 % |
| measurement | 6 | 0 % |
| super | 6 | 0 % |
| inlet | 6 | 0 % |
| injector | 6 | 0 % |
| skew | 6 | 0 % |
| radius | 6 | 0 % |
| formed | 6 | 0 % |
| 2001 | 6 | 0 % |
| oscillating | 6 | 0 % |
| law | 6 | 0 % |
| papers | 6 | 0 % |
| sae | 6 | 0 % |
| rocket | 6 | 0 % |
| young | 6 | 0 % |
| pictures | 6 | 0 % |
| 3d | 6 | 0 % |
| npsh | 6 | 0 % |
| numeca | 6 | 0 % |
| thrusters | 6 | 0 % |
| vibration | 6 | 0 % |
| barnaby | 6 | 0 % |
| problems | 6 | 0 % |
| body | 6 | 0 % |
| using | 6 | 0 % |
| single | 6 | 0 % |
| chahine | 6 | 0 % |
| et | 6 | 0 % |
| turbulence | 6 | 0 % |
| steel | 6 | 0 % |
| navier | 6 | 0 % |
| supercavity | 6 | 0 % |
| submerged | 6 | 0 % |
| air | 6 | 0 % |
| turbopump | 5 | 0 % |
| energy | 5 | 0 % |
| scaling | 5 | 0 % |
| author | 5 | 0 % |
| marine | 5 | 0 % |
| solid | 5 | 0 % |
| study | 5 | 0 % |
| tsujimoto | 5 | 0 % |
| supersonic | 5 | 0 % |
| azimuthal | 5 | 0 % |
| bodies | 5 | 0 % |
| vof | 5 | 0 % |
| behavior | 5 | 0 % |
| formula | 5 | 0 % |
| naca66 | 5 | 0 % |
| sound | 5 | 0 % |
| injectors | 5 | 0 % |
| visualization | 5 | 0 % |
| [pdf] | 5 | 0 % |
| butterfly | 5 | 0 % |
| turbines | 5 | 0 % |
| similarity | 5 | 0 % |
| added | 5 | 0 % |
| film | 5 | 0 % |
| are | 5 | 0 % |
| thornycroft | 5 | 0 % |
| - | 5 | 0 % |
| geometry | 5 | 0 % |
| diagram | 5 | 0 % |
| development | 5 | 0 % |
| siam | 5 | 0 % |
| spillway | 5 | 0 % |
| size | 5 | 0 % |
| spray | 5 | 0 % |
| separation | 5 | 0 % |
| signal | 5 | 0 % |
| cloud | 5 | 0 % |
| investigation | 5 | 0 % |
| a. | 5 | 0 % |
| valve | 5 | 0 % |
| curve | 5 | 0 % |
| induced | 5 | 0 % |
| cav | 5 | 0 % |
| instabilities | 5 | 0 % |
| parsons | 5 | 0 % |
| micro | 5 | 0 % |
| kuiper | 5 | 0 % |
| franc | 5 | 0 % |
| drop | 5 | 0 % |
| 1895 | 5 | 0 % |
| leading | 5 | 0 % |
| effects | 5 | 0 % |
| sonoluminescence | 5 | 0 % |
| projectile | 4 | 0 % |
| horn | 4 | 0 % |
| wall | 4 | 0 % |
| 1989 | 4 | 0 % |
| photograph | 4 | 0 % |
| prop | 4 | 0 % |
| plates | 4 | 0 % |
| different | 4 | 0 % |
| vertical | 4 | 0 % |
| type | 4 | 0 % |
| trailing | 4 | 0 % |
| grid | 4 | 0 % |
| vortices | 4 | 0 % |
| drag | 4 | 0 % |
| ittc | 4 | 0 % |
| nuclei | 4 | 0 % |
| bell | 4 | 0 % |
| parameter | 4 | 0 % |
| scale | 4 | 0 % |
| emission | 4 | 0 % |
| naca66-415 | 4 | 0 % |
| photo | 4 | 0 % |
| hull | 4 | 0 % |
| savchenko | 4 | 0 % |
| fluids | 4 | 0 % |
| index | 4 | 0 % |
| 1995 | 4 | 0 % |
| impact | 4 | 0 % |
| free | 4 | 0 % |
| aisi | 4 | 0 % |
| oil | 4 | 0 % |
| loading | 4 | 0 % |
| vessel | 4 | 0 % |
| theory | 4 | 0 % |
| engine | 4 | 0 % |
| inside | 4 | 0 % |
| force | 4 | 0 % |
| strouhal | 4 | 0 % |
| pvdf | 4 | 0 % |
| turbulent | 4 | 0 % |
| thesis | 4 | 0 % |
| mixture | 4 | 0 % |
| mechanism | 4 | 0 % |
| apparatus | 4 | 0 % |
| maneuvering | 4 | 0 % |
| engineering | 4 | 0 % |
| 1997 | 4 | 0 % |
| characteristics | 4 | 0 % |
| swirl | 4 | 0 % |
| setup | 4 | 0 % |
| blades | 4 | 0 % |
| vapour | 4 | 0 % |
| tests | 4 | 0 % |
| airfoil | 4 | 0 % |
| area | 4 | 0 % |
| thrust | 4 | 0 % |
| baghdassarian | 4 | 0 % |
| configuration | 4 | 0 % |
| simple | 4 | 0 % |
| towing | 4 | 0 % |
| stop | 4 | 0 % |
| multi | 4 | 0 % |
| calculations | 3 | 0 % |
| shapes | 3 | 0 % |
| system | 3 | 0 % |
| 4th | 3 | 0 % |
| ganippa | 3 | 0 % |
| froude | 3 | 0 % |
| rake | 3 | 0 % |
| transducer | 3 | 0 % |
| change | 3 | 0 % |
| joussellin | 3 | 0 % |
| influence | 3 | 0 % |
| ratio | 3 | 0 % |
| causes | 3 | 0 % |
| compressor | 3 | 0 % |
| about | 3 | 0 % |
| ring | 3 | 0 % |
| pumping | 3 | 0 % |
| oscillation | 3 | 0 % |
| relations | 3 | 0 % |
| technical | 3 | 0 % |
| y | 3 | 0 % |
| super-cavitation | 3 | 0 % |
| due | 3 | 0 % |
| intitle | 3 | 0 % |
| valve; | 3 | 0 % |
| webkr | 3 | 0 % |
| line | 3 | 0 % |
| utilization | 3 | 0 % |
| detection | 3 | 0 % |
| transfer | 3 | 0 % |
| motion | 3 | 0 % |
| merkle | 3 | 0 % |
| arndt | 3 | 0 % |
| or | 3 | 0 % |
| fortes | 3 | 0 % |
| disk | 3 | 0 % |
| compressible | 3 | 0 % |
| interaction | 3 | 0 % |
| research | 3 | 0 % |
| diatomic | 3 | 0 % |
| reboud | 3 | 0 % |
| code | 3 | 0 % |
| waves | 3 | 0 % |
| technology | 3 | 0 % |
| attack | 3 | 0 % |
| strength | 3 | 0 % |
| systems | 3 | 0 % |
| achkinadze | 3 | 0 % |
| impellers | 3 | 0 % |
| control | 3 | 0 % |
| gradient | 3 | 0 % |
| discharge | 3 | 0 % |
| axisymmetric | 3 | 0 % |
| behaviour | 3 | 0 % |
| applications | 3 | 0 % |
| scheme | 3 | 0 % |
| laser-induced | 3 | 0 % |
| tanguay | 3 | 0 % |
| physics | 3 | 0 % |
| cavitation; | 3 | 0 % |
| linearized | 3 | 0 % |
| meter | 3 | 0 % |
| approach | 3 | 0 % |
| dimension | 3 | 0 % |
| compressibility | 3 | 0 % |
| semenenko | 3 | 0 % |
| throat | 3 | 0 % |
| downstream | 3 | 0 % |
| fourth | 3 | 0 % |
| pulsating | 3 | 0 % |
| temperature | 3 | 0 % |
| formation | 3 | 0 % |
| damping | 3 | 0 % |
| tube | 3 | 0 % |
| logvinovich | 3 | 0 % |
| gas | 3 | 0 % |
| forces | 3 | 0 % |
| crash | 3 | 0 % |
| guide | 3 | 0 % |
| s | 3 | 0 % |
| ... | 3 | 0 % |
| partial | 3 | 0 % |
| nitrogen | 3 | 0 % |
| wear | 3 | 0 % |
| testing | 3 | 0 % |
| coordinates | 3 | 0 % |
| phenomena | 3 | 0 % |
| loss | 3 | 0 % |
| level | 3 | 0 % |
| efficiency | 3 | 0 % |
| propagation | 3 | 0 % |
| krasilnikov | 3 | 0 % |
| duttweiler | 3 | 0 % |
| calculate | 3 | 0 % |
| near | 3 | 0 % |
| first | 3 | 0 % |
| nscbc | 3 | 0 % |
| al. | 3 | 0 % |
| leakage | 3 | 0 % |
| charles | 2 | 0 % |
| n. | 2 | 0 % |
| materials | 2 | 0 % |
| emerson | 2 | 0 % |
| liquid-vapour | 2 | 0 % |
| equilibrium | 2 | 0 % |
| thermodynamic | 2 | 0 % |
| incipient | 2 | 0 % |
| yuriy | 2 | 0 % |
| shockwave | 2 | 0 % |
| bernoulli | 2 | 0 % |
| supercavities | 2 | 0 % |
| polytropic | 2 | 0 % |
| helical | 2 | 0 % |
| fact | 2 | 0 % |
| dang | 2 | 0 % |
| http | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| only | 2 | 0 % |
| iee1394 | 2 | 0 % |
| re | 2 | 0 % |
| algorithms | 2 | 0 % |
| problem | 2 | 0 % |
| proceedings | 2 | 0 % |
| incompressible | 2 | 0 % |
| moving | 2 | 0 % |
| vaidya | 2 | 0 % |
| irregularities | 2 | 0 % |
| s.w. | 2 | 0 % |
| c. | 2 | 0 % |
| 1015 | 2 | 0 % |
| heat | 2 | 0 % |
| invicid | 2 | 0 % |
| propulsor | 2 | 0 % |
| rate | 2 | 0 % |
| perspectives | 2 | 0 % |
| .hao | 2 | 0 % |
| piping | 2 | 0 % |
| density | 2 | 0 % |
| z | 2 | 0 % |
| source | 2 | 0 % |
| series | 2 | 0 % |
| spectra | 2 | 0 % |
| making | 2 | 0 % |
| multi-dimensional | 2 | 0 % |
| mouth | 2 | 0 % |
| meeting | 2 | 0 % |
| thickness | 2 | 0 % |
| cryogenics | 2 | 0 % |
| 0012 | 2 | 0 % |
| artificial | 2 | 0 % |
| state | 2 | 0 % |
| occurs | 2 | 0 % |
| fluctuations | 2 | 0 % |
| step | 2 | 0 % |
| pitch | 2 | 0 % |
| taylor | 2 | 0 % |
| swept | 2 | 0 % |
| axial | 2 | 0 % |
| hydraulics | 2 | 0 % |
| flat | 2 | 0 % |
| wing | 2 | 0 % |
| 4412 | 2 | 0 % |
| increase | 2 | 0 % |
| naca0020 | 2 | 0 % |
| point | 2 | 0 % |
| fedsm97-3272 | 2 | 0 % |
| horseshoe | 2 | 0 % |
| eulerian | 2 | 0 % |
| normal | 2 | 0 % |
| leonard | 2 | 0 % |
| imperfection | 2 | 0 % |
| regiane | 2 | 0 % |
| cone | 2 | 0 % |
| sump | 2 | 0 % |
| mccormick | 2 | 0 % |
| improved | 2 | 0 % |
| dimensional | 2 | 0 % |
| patella | 2 | 0 % |
| quality | 2 | 0 % |
| g. | 2 | 0 % |
| lecture | 2 | 0 % |
| hovercraft | 2 | 0 % |
| astm | 2 | 0 % |
| length | 2 | 0 % |
| kamewa | 2 | 0 % |
| concepts | 2 | 0 % |
| two-phase | 2 | 0 % |
| fujii | 2 | 0 % |
| curvilinear | 2 | 0 % |
| uhlman | 2 | 0 % |
| past | 2 | 0 % |
| acosta | 2 | 0 % |
| experment | 2 | 0 % |
| summer | 2 | 0 % |
| c | 2 | 0 % |
| lockwood | 2 | 0 % |
| skewed | 2 | 0 % |
| usn | 2 | 0 % |
| formulation | 2 | 0 % |
| planing | 2 | 0 % |
| wedge | 2 | 0 % |
| laser-induced... | 2 | 0 % |
| singhal | 2 | 0 % |
| features | 2 | 0 % |
| through | 2 | 0 % |
| molecular | 2 | 0 % |
| cav2001.library.caltech.edu/191/00/a7005.pdf | 2 | 0 % |
| lo | 2 | 0 % |
| sir | 2 | 0 % |
| transition | 2 | 0 % |
| droplets | 2 | 0 % |
| mikael | 2 | 0 % |
| observations | 2 | 0 % |
| inducers | 2 | 0 % |
| voltage | 2 | 0 % |
| ventilated | 2 | 0 % |
| function | 2 | 0 % |
| bearing | 2 | 0 % |
| channel | 2 | 0 % |
| advantages | 2 | 0 % |
| akira | 2 | 0 % |
| constant | 2 | 0 % |
| large | 2 | 0 % |
| wake | 2 | 0 % |
| david | 2 | 0 % |
| stft | 2 | 0 % |
| stepped | 2 | 0 % |
| organic | 2 | 0 % |
| brennen | 2 | 0 % |
| field | 2 | 0 % |
| location | 2 | 0 % |
| v | 2 | 0 % |
| estimation | 2 | 0 % |
| 215 | 2 | 0 % |
| diffusion | 2 | 0 % |
| reynolds | 2 | 0 % |
| shape | 2 | 0 % |
| fortes-patella | 2 | 0 % |
| . | 2 | 0 % |
| o- | 2 | 0 % |
| naca4412 | 2 | 0 % |
| naca0012 | 2 | 0 % |
| application | 2 | 0 % |
| videos | 2 | 0 % |
| experiments | 2 | 0 % |
| vs | 2 | 0 % |
| parallel | 2 | 0 % |
| heavy | 2 | 0 % |
| pressute | 2 | 0 % |
| shrink | 2 | 0 % |
| cylindrical | 2 | 0 % |
| flashing | 2 | 0 % |
| evaluate | 2 | 0 % |
| nozzles | 2 | 0 % |
| divergent | 2 | 0 % |
| sigma | 2 | 0 % |
| operating | 2 | 0 % |
| image | 2 | 0 % |
| fragmentation | 2 | 0 % |
| fft | 2 | 0 % |
| fuel | 2 | 0 % |
| zwick | 2 | 0 % |
| bellmouth | 2 | 0 % |
| gp-mf | 2 | 0 % |
| injection | 2 | 0 % |
| begining | 2 | 0 % |
| lagrangian | 2 | 0 % |
| data | 2 | 0 % |
| values | 2 | 0 % |
| kunz | 2 | 0 % |
| densities | 2 | 0 % |
| bem | 2 | 0 % |
| boats | 2 | 0 % |
| flowfield | 2 | 0 % |
| shear | 2 | 0 % |
| ultrasound | 2 | 0 % |
| 552 | 2 | 0 % |
| piezoelectric | 2 | 0 % |
| hub | 2 | 0 % |
| mechanical | 2 | 0 % |
| difference | 2 | 0 % |
| foam | 2 | 0 % |
| stage | 2 | 0 % |
| specific | 2 | 0 % |
| section | 2 | 0 % |
| needle | 2 | 0 % |
| japikse | 2 | 0 % |
| side | 2 | 0 % |
| starcd | 2 | 0 % |
| shaped | 2 | 0 % |
| rudders | 2 | 0 % |
| 2-d | 2 | 0 % |
| gap | 2 | 0 % |
| haemolysis | 2 | 0 % |
| orthogonal | 2 | 0 % |
| duration | 2 | 0 % |
| chimera | 2 | 0 % |
| f-avellan | 2 | 0 % |
| three | 2 | 0 % |
| s55c | 2 | 0 % |
| transient | 2 | 0 % |
| use | 2 | 0 % |
| venturi | 2 | 0 % |
| reference | 2 | 0 % |
| upper | 2 | 0 % |
| sspa | 2 | 0 % |
| kutta | 2 | 0 % |
| viscous | 2 | 0 % |
| view | 2 | 0 % |
| k. | 2 | 0 % |
| radial | 2 | 0 % |
| correction | 2 | 0 % |
| specifications | 2 | 0 % |
| schnerr | 2 | 0 % |
| lu | 2 | 0 % |
| turbo | 2 | 0 % |
| iteration | 2 | 0 % |
| typical | 2 | 0 % |
| computation | 2 | 0 % |
| d. | 2 | 0 % |
| stream | 2 | 0 % |
| full | 2 | 0 % |
| limit | 2 | 0 % |
| bearings | 2 | 0 % |
| response | 2 | 0 % |
| labview | 2 | 0 % |
| watanabe | 2 | 0 % |
| condition | 2 | 0 % |
| sonochemistry | 2 | 0 % |
| potential | 2 | 0 % |
| validation | 2 | 0 % |
| mark | 2 | 0 % |
| sharp | 2 | 0 % |
| characteristic | 2 | 0 % |
| keller | 2 | 0 % |
| region | 2 | 0 % |
| slamming | 2 | 0 % |
| circular | 2 | 0 % |
| grekula | 2 | 0 % |
| division | 2 | 0 % |
| installation | 2 | 0 % |
| f.c. | 2 | 0 % |
| homogeneous | 2 | 0 % |
| r.f. | 2 | 0 % |
| 66 | 2 | 0 % |
| beam | 2 | 0 % |
| material | 2 | 0 % |
| usa | 2 | 0 % |
| 1055 | 2 | 0 % |
| consumption | 2 | 0 % |
| this | 2 | 0 % |
| lifting | 2 | 0 % |
| high-speed | 2 | 0 % |
| 1998 | 2 | 0 % |
| preconditioning | 2 | 0 % |
| navsea | 2 | 0 % |
| studies | 2 | 0 % |
| structure | 2 | 0 % |
| implementation | 1 | 0 % |
| chebyshev | 1 | 0 % |
| load | 1 | 0 % |
| particle | 1 | 0 % |
| rotation | 1 | 0 % |
| forming | 1 | 0 % |
| light | 1 | 0 % |
| pressure-velocity-density | 1 | 0 % |
| rigid | 1 | 0 % |
| heatin | 1 | 0 % |
| happen | 1 | 0 % |
| molecule | 1 | 0 % |
| rule | 1 | 0 % |
| cryogen | 1 | 0 % |
| explained | 1 | 0 % |
| 1969 | 1 | 0 % |
| can | 1 | 0 % |
| yoshinobu | 1 | 0 % |
| curves | 1 | 0 % |
| where | 1 | 0 % |
| choked | 1 | 0 % |
| o-type | 1 | 0 % |
| kubota | 1 | 0 % |
| coefficients | 1 | 0 % |
| arc | 1 | 0 % |
| riemann | 1 | 0 % |
| jacques | 1 | 0 % |
| inch | 1 | 0 % |
| runner | 1 | 0 % |
| sweep | 1 | 0 % |
| astolfi | 1 | 0 % |
| dipoles | 1 | 0 % |
| dynamical | 1 | 0 % |
| mechanics | 1 | 0 % |
| -combustion | 1 | 0 % |
| spheroidal | 1 | 0 % |
| fatigue | 1 | 0 % |
| avoid | 1 | 0 % |
| nk | 1 | 0 % |
| pelton | 1 | 0 % |
| laminar | 1 | 0 % |
| excitation | 1 | 0 % |
| А | 1 | 0 % |
| taib | 1 | 0 % |
| flowmeter | 1 | 0 % |
| inlet. | 1 | 0 % |
| vapor | 1 | 0 % |
| explosion | 1 | 0 % |
| weber | 1 | 0 % |
| experimentation | 1 | 0 % |
| lift | 1 | 0 % |
| naca0015 | 1 | 0 % |
| 415 | 1 | 0 % |
| measuring | 1 | 0 % |
| into | 1 | 0 % |
| transducers | 1 | 0 % |
| 135-141 | 1 | 0 % |
| peening | 1 | 0 % |
| rpe | 1 | 0 % |
| hydrodinamic | 1 | 0 % |
| 3% | 1 | 0 % |
| blunt | 1 | 0 % |
| configurations | 1 | 0 % |
| multi-hole | 1 | 0 % |
| few | 1 | 0 % |
| kidneys | 1 | 0 % |
| plunger | 1 | 0 % |
| swim | 1 | 0 % |
| cav2001.library.caltech.edu/358/00/b8_006_nagahara.pdf | 1 | 0 % |
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| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx?????????? | 1 | 0 % |
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| Other words | 421 | 6.4 % |