| 1551 different keywords | Search | Percent |
|---|
| cavitation | 581 | 8.1 % |
| of | 234 | 3.2 % |
| pdf | 172 | 2.4 % |
| in | 125 | 1.7 % |
| propeller | 123 | 1.7 % |
| pump | 117 | 1.6 % |
| orifice | 84 | 1.1 % |
| centrifugal | 83 | 1.1 % |
| flow | 82 | 1.1 % |
| and | 78 | 1 % |
| bubble | 76 | 1 % |
| a | 75 | 1 % |
| the | 75 | 1 % |
| fluent | 73 | 1 % |
| vortex | 64 | 0.9 % |
| numerical | 63 | 0.8 % |
| on | 59 | 0.8 % |
| restriction | 57 | 0.8 % |
| pressure | 52 | 0.7 % |
| filetype | 51 | 0.7 % |
| for | 51 | 0.7 % |
| hydrofoil | 47 | 0.6 % |
| water | 47 | 0.6 % |
| model | 45 | 0.6 % |
| method | 44 | 0.6 % |
| jet | 40 | 0.5 % |
| bubbles | 36 | 0.5 % |
| supercavitating | 35 | 0.4 % |
| nozzle | 35 | 0.4 % |
| supercavitation | 34 | 0.4 % |
| ship | 34 | 0.4 % |
| simulation | 31 | 0.4 % |
| pumps | 31 | 0.4 % |
| cavitating | 30 | 0.4 % |
| design | 30 | 0.4 % |
| propellers | 27 | 0.3 % |
| turbine | 25 | 0.3 % |
| rudder | 25 | 0.3 % |
| erosion | 24 | 0.3 % |
| boundary | 24 | 0.3 % |
| modeling | 24 | 0.3 % |
| cavity | 24 | 0.3 % |
| cfd | 24 | 0.3 % |
| calculation | 24 | 0.3 % |
| dynamics | 23 | 0.3 % |
| distribution | 22 | 0.3 % |
| analysis | 22 | 0.3 % |
| flows | 22 | 0.3 % |
| inducer | 22 | 0.3 % |
| frequency | 22 | 0.3 % |
| kaplan | 22 | 0.3 % |
| tunnel | 20 | 0.2 % |
| azipod | 19 | 0.2 % |
| study | 19 | 0.2 % |
| how | 19 | 0.2 % |
| speed | 19 | 0.2 % |
| experimental | 19 | 0.2 % |
| equation | 18 | 0.2 % |
| noise | 18 | 0.2 % |
| test | 17 | 0.2 % |
| unsteady | 17 | 0.2 % |
| to | 17 | 0.2 % |
| valve | 17 | 0.2 % |
| near | 17 | 0.2 % |
| solid | 16 | 0.2 % |
| submerged | 16 | 0.2 % |
| high | 16 | 0.2 % |
| is | 15 | 0.2 % |
| blade | 15 | 0.2 % |
| velocity | 15 | 0.2 % |
| impeller | 15 | 0.2 % |
| diesel | 15 | 0.2 % |
| suction | 15 | 0.2 % |
| by | 14 | 0.1 % |
| surface | 14 | 0.1 % |
| stokes | 14 | 0.1 % |
| boundaries | 14 | 0.1 % |
| orifices | 14 | 0.1 % |
| 2d | 14 | 0.1 % |
| marine | 13 | 0.1 % |
| injector | 13 | 0.1 % |
| symposium | 13 | 0.1 % |
| laser | 13 | 0.1 % |
| with | 13 | 0.1 % |
| types | 13 | 0.1 % |
| naca | 13 | 0.1 % |
| strength | 13 | 0.1 % |
| plate | 13 | 0.1 % |
| international | 13 | 0.1 % |
| phase | 12 | 0.1 % |
| number | 12 | 0.1 % |
| pipe | 12 | 0.1 % |
| thesis | 12 | 0.1 % |
| wave | 12 | 0.1 % |
| two | 12 | 0.1 % |
| sheet | 12 | 0.1 % |
| modelling | 12 | 0.1 % |
| turbopump | 11 | 0.1 % |
| experiment | 11 | 0.1 % |
| butterfly | 11 | 0.1 % |
| rocket | 11 | 0.1 % |
| characteristics | 11 | 0.1 % |
| effects | 11 | 0.1 % |
| air | 11 | 0.1 % |
| piercing | 11 | 0.1 % |
| what | 10 | 0.1 % |
| underwater | 10 | 0.1 % |
| horn | 10 | 0.1 % |
| video | 10 | 0.1 % |
| liquid | 10 | 0.1 % |
| coefficient | 10 | 0.1 % |
| free | 10 | 0.1 % |
| navier | 10 | 0.1 % |
| induced | 10 | 0.1 % |
| effect | 10 | 0.1 % |
| behavior | 9 | 0.1 % |
| cavitator | 9 | 0.1 % |
| rotating | 9 | 0.1 % |
| foil | 9 | 0.1 % |
| turbomachinery | 9 | 0.1 % |
| crum | 9 | 0.1 % |
| npsh | 9 | 0.1 % |
| time | 9 | 0.1 % |
| spherical | 9 | 0.1 % |
| tensile | 9 | 0.1 % |
| turbin | 9 | 0.1 % |
| prediction | 9 | 0.1 % |
| investigation | 9 | 0.1 % |
| cav | 9 | 0.1 % |
| lattice | 9 | 0.1 % |
| equilibrium | 8 | 0.1 % |
| system | 8 | 0.1 % |
| incipient | 8 | 0.1 % |
| journal | 8 | 0.1 % |
| instability | 8 | 0.1 % |
| models | 8 | 0.1 % |
| scale | 8 | 0.1 % |
| acoustic | 8 | 0.1 % |
| tip | 8 | 0.1 % |
| ventilated | 8 | 0.1 % |
| wake | 8 | 0.1 % |
| arndt | 8 | 0.1 % |
| pictures | 8 | 0.1 % |
| 1979 | 8 | 0.1 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 8 | 0.1 % |
| using | 8 | 0.1 % |
| cloud | 8 | 0.1 % |
| paolo | 8 | 0.1 % |
| cavitations | 8 | 0.1 % |
| calculate | 8 | 0.1 % |
| rayleigh | 8 | 0.1 % |
| energy | 7 | 0 % |
| computational | 7 | 0 % |
| type | 7 | 0 % |
| heat | 7 | 0 % |
| lift | 7 | 0 % |
| bell | 7 | 0 % |
| collapse | 7 | 0 % |
| performance | 7 | 0 % |
| & | 7 | 0 % |
| hull | 7 | 0 % |
| 2001 | 7 | 0 % |
| over | 7 | 0 % |
| skewed | 7 | 0 % |
| through | 7 | 0 % |
| sizing | 7 | 0 % |
| damage | 7 | 0 % |
| research | 7 | 0 % |
| 3d | 7 | 0 % |
| j. | 7 | 0 % |
| waves | 7 | 0 % |
| data | 7 | 0 % |
| 0015 | 7 | 0 % |
| vibration | 7 | 0 % |
| shedding | 7 | 0 % |
| shock | 7 | 0 % |
| gas | 7 | 0 % |
| thrust | 7 | 0 % |
| condition | 7 | 0 % |
| plesset | 7 | 0 % |
| joint | 7 | 0 % |
| homogeneous | 7 | 0 % |
| at | 7 | 0 % |
| author | 6 | 0 % |
| euler | 6 | 0 % |
| fluid | 6 | 0 % |
| navier-stokes | 6 | 0 % |
| explosion | 6 | 0 % |
| partially | 6 | 0 % |
| naca0015 | 6 | 0 % |
| axial | 6 | 0 % |
| introduction | 6 | 0 % |
| savchenko | 6 | 0 % |
| intitle | 6 | 0 % |
| panel | 6 | 0 % |
| hydrodynamic | 6 | 0 % |
| sae | 6 | 0 % |
| motion | 6 | 0 % |
| lithotripsy | 6 | 0 % |
| an | 6 | 0 % |
| atlar | 6 | 0 % |
| edge | 6 | 0 % |
| cav2001 | 6 | 0 % |
| expansion | 6 | 0 % |
| power | 6 | 0 % |
| code | 6 | 0 % |
| nozzles | 6 | 0 % |
| tank | 6 | 0 % |
| geometry | 6 | 0 % |
| development | 6 | 0 % |
| boncinelli | 6 | 0 % |
| body | 6 | 0 % |
| single | 6 | 0 % |
| new | 6 | 0 % |
| damping | 6 | 0 % |
| integral | 6 | 0 % |
| hydraulic | 6 | 0 % |
| spectrum | 6 | 0 % |
| keller | 6 | 0 % |
| tomita | 5 | 0 % |
| super | 5 | 0 % |
| inlet | 5 | 0 % |
| vapor | 5 | 0 % |
| density | 5 | 0 % |
| rayleigh-plesset | 5 | 0 % |
| ring | 5 | 0 % |
| formed | 5 | 0 % |
| reentrant | 5 | 0 % |
| sound | 5 | 0 % |
| hydrodynamics | 5 | 0 % |
| paper | 5 | 0 % |
| hydrofoils | 5 | 0 % |
| parameters | 5 | 0 % |
| djeridi | 5 | 0 % |
| layer | 5 | 0 % |
| solution | 5 | 0 % |
| transfer | 5 | 0 % |
| angle | 5 | 0 % |
| field | 5 | 0 % |
| shape | 5 | 0 % |
| compressible | 5 | 0 % |
| force | 5 | 0 % |
| multiphase | 5 | 0 % |
| diagram | 5 | 0 % |
| behaviour | 5 | 0 % |
| element | 5 | 0 % |
| hosangadi | 5 | 0 % |
| size | 5 | 0 % |
| methods | 5 | 0 % |
| blades | 5 | 0 % |
| volume | 5 | 0 % |
| turbulence | 5 | 0 % |
| dynamic | 5 | 0 % |
| head | 5 | 0 % |
| s | 5 | 0 % |
| around | 5 | 0 % |
| ships | 5 | 0 % |
| inception | 5 | 0 % |
| towing | 5 | 0 % |
| measurement | 4 | 0 % |
| scaling | 4 | 0 % |
| wall | 4 | 0 % |
| sauer | 4 | 0 % |
| plates | 4 | 0 % |
| different | 4 | 0 % |
| vertical | 4 | 0 % |
| runner | 4 | 0 % |
| vortices | 4 | 0 % |
| equations | 4 | 0 % |
| drag | 4 | 0 % |
| perspectives | 4 | 0 % |
| kavitation | 4 | 0 % |
| mouth | 4 | 0 % |
| ratio | 4 | 0 % |
| intake | 4 | 0 % |
| artificial | 4 | 0 % |
| state | 4 | 0 % |
| nuclei | 4 | 0 % |
| mass | 4 | 0 % |
| 1973 | 4 | 0 % |
| vof | 4 | 0 % |
| formula | 4 | 0 % |
| diffuser | 4 | 0 % |
| quality | 4 | 0 % |
| naval | 4 | 0 % |
| cascade | 4 | 0 % |
| length | 4 | 0 % |
| index | 4 | 0 % |
| two-phase | 4 | 0 % |
| oil | 4 | 0 % |
| distance | 4 | 0 % |
| non-spherical | 4 | 0 % |
| vessel | 4 | 0 % |
| fortes | 4 | 0 % |
| theory | 4 | 0 % |
| reynolds | 4 | 0 % |
| solver | 4 | 0 % |
| are | 4 | 0 % |
| naca4412 | 4 | 0 % |
| history | 4 | 0 % |
| turbulent | 4 | 0 % |
| steady | 4 | 0 % |
| attack | 4 | 0 % |
| - | 4 | 0 % |
| rebound | 4 | 0 % |
| systems | 4 | 0 % |
| mechanism | 4 | 0 % |
| bem | 4 | 0 % |
| tab_hty | 4 | 0 % |
| applications | 4 | 0 % |
| work | 4 | 0 % |
| et | 4 | 0 % |
| transient | 4 | 0 % |
| use | 4 | 0 % |
| francis | 4 | 0 % |
| kutta | 4 | 0 % |
| conclusion | 4 | 0 % |
| tube | 4 | 0 % |
| supercavitation-problems | 4 | 0 % |
| schnerr | 4 | 0 % |
| bubbly | 4 | 0 % |
| rarefaction | 4 | 0 % |
| nitrogen | 4 | 0 % |
| hsva | 4 | 0 % |
| luminescence | 4 | 0 % |
| potential | 4 | 0 % |
| level | 4 | 0 % |
| simple | 4 | 0 % |
| vehicle | 4 | 0 % |
| vs. | 4 | 0 % |
| from | 4 | 0 % |
| kjeldsen | 4 | 0 % |
| robert | 4 | 0 % |
| material | 4 | 0 % |
| dumont | 4 | 0 % |
| vorticity | 4 | 0 % |
| kuklinski | 4 | 0 % |
| barotropic | 4 | 0 % |
| nexearch | 4 | 0 % |
| diameter | 4 | 0 % |
| calculations | 3 | 0 % |
| shapes | 3 | 0 % |
| light | 3 | 0 % |
| shockwave | 3 | 0 % |
| sumulations | 3 | 0 % |
| 1999 | 3 | 0 % |
| nucleation | 3 | 0 % |
| 2-d | 3 | 0 % |
| trailing | 3 | 0 % |
| c. | 3 | 0 % |
| laminar | 3 | 0 % |
| rate | 3 | 0 % |
| henda | 3 | 0 % |
| conditions | 3 | 0 % |
| source | 3 | 0 % |
| into | 3 | 0 % |
| tsujimoto | 3 | 0 % |
| pitch | 3 | 0 % |
| about | 3 | 0 % |
| r. | 3 | 0 % |
| parameter | 3 | 0 % |
| considerations | 3 | 0 % |
| flat | 3 | 0 % |
| oxygen | 3 | 0 % |
| pumping | 3 | 0 % |
| radius | 3 | 0 % |
| oscillation | 3 | 0 % |
| georges | 3 | 0 % |
| regiane | 3 | 0 % |
| sump | 3 | 0 % |
| soyama | 3 | 0 % |
| newman | 3 | 0 % |
| lertnuwat | 3 | 0 % |
| dimensional | 3 | 0 % |
| patella | 3 | 0 % |
| schematic | 3 | 0 % |
| ellipse | 3 | 0 % |
| valves | 3 | 0 % |
| template | 3 | 0 % |
| turbines | 3 | 0 % |
| runge | 3 | 0 % |
| similarity | 3 | 0 % |
| observations | 3 | 0 % |
| developed | 3 | 0 % |
| measurements | 3 | 0 % |
| propulsion | 3 | 0 % |
| time-frequency | 3 | 0 % |
| non | 3 | 0 % |
| capture | 3 | 0 % |
| or | 3 | 0 % |
| kinnas | 3 | 0 % |
| x | 3 | 0 % |
| autospectrum | 3 | 0 % |
| tullis | 3 | 0 % |
| inside | 3 | 0 % |
| intakes | 3 | 0 % |
| physical | 3 | 0 % |
| between | 3 | 0 % |
| application | 3 | 0 % |
| space | 3 | 0 % |
| olofsson | 3 | 0 % |
| comparison | 3 | 0 % |
| 2000 | 3 | 0 % |
| review | 3 | 0 % |
| narrow | 3 | 0 % |
| order | 3 | 0 % |
| casing | 3 | 0 % |
| des | 3 | 0 % |
| spillway | 3 | 0 % |
| content | 3 | 0 % |
| kato | 3 | 0 % |
| axisymmetric | 3 | 0 % |
| difference | 3 | 0 % |
| behind | 3 | 0 % |
| lichtarowicz | 3 | 0 % |
| section | 3 | 0 % |
| turbomachines | 3 | 0 % |
| chahine | 3 | 0 % |
| gap | 3 | 0 % |
| compressibility | 3 | 0 % |
| balance | 3 | 0 % |
| cavitaion | 3 | 0 % |
| modern | 3 | 0 % |
| .pdf | 3 | 0 % |
| simulations | 3 | 0 % |
| fourth | 3 | 0 % |
| cavities | 3 | 0 % |
| .edu | 3 | 0 % |
| viscous | 3 | 0 % |
| airfoil | 3 | 0 % |
| formation | 3 | 0 % |
| a. | 3 | 0 % |
| curve | 3 | 0 % |
| ultrasonic | 3 | 0 % |
| dam | 3 | 0 % |
| coordinates | 3 | 0 % |
| niklas | 3 | 0 % |
| franc | 3 | 0 % |
| site | 3 | 0 % |
| ashvin | 3 | 0 % |
| morten | 3 | 0 % |
| preconditioned | 3 | 0 % |
| leading | 3 | 0 % |
| abstract | 3 | 0 % |
| 3 | 3 | 0 % |
| hykat | 3 | 0 % |
| multi | 3 | 0 % |
| slender | 3 | 0 % |
| rough | 2 | 0 % |
| projectile | 2 | 0 % |
| iwai | 2 | 0 % |
| particle | 2 | 0 % |
| karman | 2 | 0 % |
| counterjet | 2 | 0 % |
| time“ | 2 | 0 % |
| practical | 2 | 0 % |
| heaters | 2 | 0 % |
| fraction | 2 | 0 % |
| yuriy | 2 | 0 % |
| press | 2 | 0 % |
| bernoulli | 2 | 0 % |
| jets | 2 | 0 % |
| procedure | 2 | 0 % |
| momma | 2 | 0 % |
| ganippa | 2 | 0 % |
| can | 2 | 0 % |
| prop | 2 | 0 % |
| qian | 2 | 0 % |
| hardness | 2 | 0 % |
| helical | 2 | 0 % |
| incidence | 2 | 0 % |
| coefficients | 2 | 0 % |
| static | 2 | 0 % |
| lindau | 2 | 0 % |
| cause | 2 | 0 % |
| maps | 2 | 0 % |
| mechanics | 2 | 0 % |
| caltech | 2 | 0 % |
| volute | 2 | 0 % |
| mohamed | 2 | 0 % |
| generators | 2 | 0 % |
| cnes | 2 | 0 % |
| 1992 | 2 | 0 % |
| efffects | 2 | 0 % |
| strip | 2 | 0 % |
| gopalan | 2 | 0 % |
| géophysiques | 2 | 0 % |
| protection | 2 | 0 % |
| width | 2 | 0 % |
| spectra | 2 | 0 % |
| series | 2 | 0 % |
| influence | 2 | 0 % |
| ca | 2 | 0 % |
| combes | 2 | 0 % |
| observation | 2 | 0 % |
| ”collapse | 2 | 0 % |
| supersonic | 2 | 0 % |
| j | 2 | 0 % |
| occurs | 2 | 0 % |
| step | 2 | 0 % |
| mesh | 2 | 0 % |
| designing | 2 | 0 % |
| algorithm | 2 | 0 % |
| oscillations | 2 | 0 % |
| tunnels | 2 | 0 % |
| hydraulics | 2 | 0 % |
| liquids | 2 | 0 % |
| rules | 2 | 0 % |
| s15c | 2 | 0 % |
| 1991 | 2 | 0 % |
| bodies | 2 | 0 % |
| shen | 2 | 0 % |
| emission | 2 | 0 % |
| sessiona6 | 2 | 0 % |
| von | 2 | 0 % |
| return | 2 | 0 % |
| blood | 2 | 0 % |
| point | 2 | 0 % |
| duffing | 2 | 0 % |
| chaotic | 2 | 0 % |
| technical | 2 | 0 % |
| lohrberg | 2 | 0 % |
| thermal | 2 | 0 % |
| 1977 | 2 | 0 % |
| visualization | 2 | 0 % |
| numericals | 2 | 0 % |
| newcastle | 2 | 0 % |
| lighthill | 2 | 0 % |
| pei | 2 | 0 % |
| g. | 2 | 0 % |
| oscillating | 2 | 0 % |
| cambridge | 2 | 0 % |
| soc. | 2 | 0 % |
| yoshida | 2 | 0 % |
| uhlman | 2 | 0 % |
| propellor | 2 | 0 % |
| impact | 2 | 0 % |
| dr. | 2 | 0 % |
| asme | 2 | 0 % |
| low | 2 | 0 % |
| liu | 2 | 0 % |
| jessup | 2 | 0 % |
| molecular | 2 | 0 % |
| mikael | 2 | 0 % |
| inducers | 2 | 0 % |
| duplex | 2 | 0 % |
| b | 2 | 0 % |
| some | 2 | 0 % |
| recirculation | 2 | 0 % |
| constant | 2 | 0 % |
| techniques | 2 | 0 % |
| spot | 2 | 0 % |
| david | 2 | 0 % |
| extents | 2 | 0 % |
| against | 2 | 0 % |
| merkle | 2 | 0 % |
| investigations | 2 | 0 % |
| does | 2 | 0 % |
| sugiyama | 2 | 0 % |
| s. | 2 | 0 % |
| engine | 2 | 0 % |
| strain | 2 | 0 % |
| zhong | 2 | 0 % |
| solve | 2 | 0 % |
| interaction | 2 | 0 % |
| equivalent | 2 | 0 % |
| young | 2 | 0 % |
| . | 2 | 0 % |
| example | 2 | 0 % |
| naca0012 | 2 | 0 % |
| reboud | 2 | 0 % |
| videos | 2 | 0 % |
| experiments | 2 | 0 % |
| podded | 2 | 0 % |
| phenomenon | 2 | 0 % |
| thierry | 2 | 0 % |
| industriels | 2 | 0 % |
| re-entrant | 2 | 0 % |
| reduction | 2 | 0 % |
| divergent | 2 | 0 % |
| modelisation | 2 | 0 % |
| fft | 2 | 0 % |
| resistance | 2 | 0 % |
| turbopumps | 2 | 0 % |
| stability | 2 | 0 % |
| methodology | 2 | 0 % |
| france | 2 | 0 % |
| headform | 2 | 0 % |
| u | 2 | 0 % |
| injection | 2 | 0 % |
| achkinadze | 2 | 0 % |
| ludwig | 2 | 0 % |
| colonius | 2 | 0 % |
| unnels | 2 | 0 % |
| circulation | 2 | 0 % |
| c. | 2 | 0 % |
| termination | 2 | 0 % |
| inertia | 2 | 0 % |
| controlled | 2 | 0 % |
| control | 2 | 0 % |
| global | 2 | 0 % |
| electrolysis | 2 | 0 % |
| as | 2 | 0 % |
| sreedhar | 2 | 0 % |
| 5 | 2 | 0 % |
| apparatus | 2 | 0 % |
| engineering | 2 | 0 % |
| hypervelocity | 2 | 0 % |
| problems | 2 | 0 % |
| hub | 2 | 0 % |
| scheme | 2 | 0 % |
| laser-induced | 2 | 0 % |
| laboratoire | 2 | 0 % |
| yin | 2 | 0 % |
| specific | 2 | 0 % |
| physics | 2 | 0 % |
| needle | 2 | 0 % |
| japikse | 2 | 0 % |
| during | 2 | 0 % |
| signal | 2 | 0 % |
| meter | 2 | 0 % |
| american | 2 | 0 % |
| approach | 2 | 0 % |
| chen | 2 | 0 % |
| technologies | 2 | 0 % |
| cavition | 2 | 0 % |
| critical | 2 | 0 % |
| prototype | 2 | 0 % |
| concept | 2 | 0 % |
| 1996 | 2 | 0 % |
| scp | 2 | 0 % |
| t | 2 | 0 % |
| asce | 2 | 0 % |
| o. | 2 | 0 % |
| guidance | 2 | 0 % |
| lakshminarayana | 2 | 0 % |
| tsubota | 2 | 0 % |
| venturi | 2 | 0 % |
| stuart | 2 | 0 % |
| backward | 2 | 0 % |
| stoffel | 2 | 0 % |
| h. | 2 | 0 % |
| tests | 2 | 0 % |
| hofmann | 2 | 0 % |
| view | 2 | 0 % |
| upwind | 2 | 0 % |
| temperature | 2 | 0 % |
| 2008 | 2 | 0 % |
| dye | 2 | 0 % |
| drawing | 2 | 0 % |
| area | 2 | 0 % |
| nicolas | 2 | 0 % |
| torque | 2 | 0 % |
| w. | 2 | 0 % |
| ann | 2 | 0 % |
| conference | 2 | 0 % |
| screw | 2 | 0 % |
| weitendorf | 2 | 0 % |
| ecoulements | 2 | 0 % |
| turbo | 2 | 0 % |
| okada.t. | 2 | 0 % |
| p. | 2 | 0 % |
| 2 | 2 | 0 % |
| convergent | 2 | 0 % |
| computation | 2 | 0 % |
| d. | 2 | 0 % |
| stream | 2 | 0 % |
| momentum | 2 | 0 % |
| 1986 | 2 | 0 % |
| lauterborn | 2 | 0 % |
| fifth | 2 | 0 % |
| j.p. | 2 | 0 % |
| partial | 2 | 0 % |
| definition | 2 | 0 % |
| i | 2 | 0 % |
| farhat | 2 | 0 % |
| mean | 2 | 0 % |
| harbor | 2 | 0 % |
| kinematic | 2 | 0 % |
| loss | 2 | 0 % |
| symmetric | 2 | 0 % |
| refrigerant | 2 | 0 % |
| supercavity | 2 | 0 % |
| automobile | 2 | 0 % |
| resistant | 2 | 0 % |
| shima | 2 | 0 % |
| grekula | 2 | 0 % |
| division | 2 | 0 % |
| drop | 2 | 0 % |
| blowdown | 2 | 0 % |
| usa | 2 | 0 % |
| 1055 | 2 | 0 % |
| sectional | 2 | 0 % |
| song | 2 | 0 % |
| aoa | 2 | 0 % |
| advance | 2 | 0 % |
| photos | 2 | 0 % |
| gabor | 2 | 0 % |
| r | 2 | 0 % |
| h | 2 | 0 % |
| picture | 2 | 0 % |
| capuani | 2 | 0 % |
| al. | 2 | 0 % |
| structure | 2 | 0 % |
| sonoluminescence | 2 | 0 % |
| riabushinsky | 1 | 0 % |
| implementation | 1 | 0 % |
| ita | 1 | 0 % |
| -gas | 1 | 0 % |
| reasons | 1 | 0 % |
| constrained | 1 | 0 % |
| geisler | 1 | 0 % |
| rigid | 1 | 0 % |
| pitting | 1 | 0 % |
| materials | 1 | 0 % |
| emerson | 1 | 0 % |
| kirschner | 1 | 0 % |
| medicine | 1 | 0 % |
| relevant | 1 | 0 % |
| previous | 1 | 0 % |
| much | 1 | 0 % |
| developments | 1 | 0 % |
| argon | 1 | 0 % |
| polytropic | 1 | 0 % |
| zur | 1 | 0 % |
| prads | 1 | 0 % |
| yoshinobu | 1 | 0 % |
| curves | 1 | 0 % |
| j.n | 1 | 0 % |
| flight | 1 | 0 % |
| average | 1 | 0 % |
| buble | 1 | 0 % |
| kubota | 1 | 0 % |
| nick | 1 | 0 % |
| k | 1 | 0 % |
| lomax | 1 | 0 % |
| self-oscillating | 1 | 0 % |
| isl | 1 | 0 % |
| kuzman-anton | 1 | 0 % |
| jet-impact | 1 | 0 % |
| viscosity | 1 | 0 % |
| astern | 1 | 0 % |
| j.s.uhlman | 1 | 0 % |
| riemann | 1 | 0 % |
| correlation | 1 | 0 % |
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| 96 | 1 | 0 % |
| coalescence | 1 | 0 % |
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| beitrag | 1 | 0 % |
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| 20.0u-pa | 1 | 0 % |
| sessiona5.003. | 1 | 0 % |
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| am. | 1 | 0 % |
| thermodynamik | 1 | 0 % |
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| multi-hole | 1 | 0 % |
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| ostwalds | 1 | 0 % |
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| chaves | 1 | 0 % |
| show | 1 | 0 % |
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| skew | 1 | 0 % |
| zzzzzzzzzzzzzzzzzzzzzzzzzzzzzzzzzzxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 1 | 0 % |
| de | 1 | 0 % |
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| mehmet | 1 | 0 % |
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| 1-100 | 1 | 0 % |
| he | 1 | 0 % |
| naca0020 | 1 | 0 % |
| facilities | 1 | 0 % |
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| jl | 1 | 0 % |
| injectors | 1 | 0 % |
| explicit | 1 | 0 % |
| 1993 | 1 | 0 % |
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| reflector | 1 | 0 % |
| courtot | 1 | 0 % |
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| w | 1 | 0 % |
| hammitt | 1 | 0 % |
| vladimir.krasilnikov | 1 | 0 % |
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| la | 1 | 0 % |
| turbinia | 1 | 0 % |
| describing | 1 | 0 % |
| break-up | 1 | 0 % |
| 1981 | 1 | 0 % |
| [pdf] | 1 | 0 % |
| hovercraft | 1 | 0 % |
| resonant | 1 | 0 % |
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| overview | 1 | 0 % |
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| fine/turbo | 1 | 0 % |
| eulerian-lagrangian | 1 | 0 % |
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| result | 1 | 0 % |
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| d.n.1960 | 1 | 0 % |
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| results | 1 | 0 % |
| Other words | 551 | 7.7 % |
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