| 1069 different keywords | Search | Percent |
|---|
| cavitation | 317 | 8.2 % |
| of | 126 | 3.2 % |
| orifice | 87 | 2.2 % |
| in | 70 | 1.8 % |
| and | 59 | 1.5 % |
| pdf | 54 | 1.4 % |
| propeller | 52 | 1.3 % |
| restriction | 50 | 1.3 % |
| pump | 50 | 1.3 % |
| analysis | 45 | 1.1 % |
| the | 42 | 1 % |
| bubble | 41 | 1 % |
| water | 39 | 1 % |
| vortex | 39 | 1 % |
| a | 37 | 0.9 % |
| joint | 33 | 0.8 % |
| flow | 32 | 0.8 % |
| on | 28 | 0.7 % |
| pressure | 26 | 0.6 % |
| erosion | 23 | 0.5 % |
| frequency | 22 | 0.5 % |
| model | 20 | 0.5 % |
| inducer | 20 | 0.5 % |
| supercavitation | 20 | 0.5 % |
| numerical | 19 | 0.4 % |
| turbine | 19 | 0.4 % |
| filetype | 19 | 0.4 % |
| noise | 19 | 0.4 % |
| time | 18 | 0.4 % |
| for | 18 | 0.4 % |
| symposium | 17 | 0.4 % |
| time-frequency | 17 | 0.4 % |
| surface | 16 | 0.4 % |
| tip | 16 | 0.4 % |
| method | 16 | 0.4 % |
| boundary | 15 | 0.3 % |
| tunnel | 15 | 0.3 % |
| simulation | 14 | 0.3 % |
| cavity | 14 | 0.3 % |
| characteristics | 14 | 0.3 % |
| centrifugal | 14 | 0.3 % |
| cav2001 | 13 | 0.3 % |
| plate | 13 | 0.3 % |
| shock | 13 | 0.3 % |
| design | 13 | 0.3 % |
| fluent | 13 | 0.3 % |
| orifices | 13 | 0.3 % |
| experimental | 13 | 0.3 % |
| dynamics | 12 | 0.3 % |
| number | 12 | 0.3 % |
| jet | 12 | 0.3 % |
| 2001 | 12 | 0.3 % |
| coefficient | 12 | 0.3 % |
| supercavitating | 12 | 0.3 % |
| types | 12 | 0.3 % |
| international | 12 | 0.3 % |
| tab_hty | 12 | 0.3 % |
| blade | 11 | 0.2 % |
| to | 11 | 0.2 % |
| cavitating | 11 | 0.2 % |
| propellers | 11 | 0.2 % |
| methods | 11 | 0.2 % |
| hydraulic | 11 | 0.2 % |
| nexearch | 11 | 0.2 % |
| piercing | 11 | 0.2 % |
| by | 10 | 0.2 % |
| study | 10 | 0.2 % |
| introduction | 10 | 0.2 % |
| butterfly | 10 | 0.2 % |
| wave | 10 | 0.2 % |
| equation | 10 | 0.2 % |
| kaplan | 10 | 0.2 % |
| submerged | 10 | 0.2 % |
| effects | 10 | 0.2 % |
| bubbles | 9 | 0.2 % |
| pipe | 9 | 0.2 % |
| panel | 9 | 0.2 % |
| quality | 9 | 0.2 % |
| hydrodynamic | 9 | 0.2 % |
| with | 9 | 0.2 % |
| rocket | 9 | 0.2 % |
| injection | 9 | 0.2 % |
| gas | 9 | 0.2 % |
| cfd | 9 | 0.2 % |
| cav | 9 | 0.2 % |
| nozzle | 9 | 0.2 % |
| air | 9 | 0.2 % |
| azipod | 8 | 0.2 % |
| solid | 8 | 0.2 % |
| paper | 8 | 0.2 % |
| vibration | 8 | 0.2 % |
| suction | 8 | 0.2 % |
| what | 7 | 0.1 % |
| turbopump | 7 | 0.1 % |
| author | 7 | 0.1 % |
| is | 7 | 0.1 % |
| speed | 7 | 0.1 % |
| applications | 7 | 0.1 % |
| vapour | 7 | 0.1 % |
| valve | 7 | 0.1 % |
| rarefaction | 7 | 0.1 % |
| effect | 7 | 0.1 % |
| calculation | 7 | 0.1 % |
| high | 7 | 0.1 % |
| measurement | 6 | 0.1 % |
| underwater | 6 | 0.1 % |
| test | 6 | 0.1 % |
| technical | 6 | 0.1 % |
| template | 6 | 0.1 % |
| lithotripsy | 6 | 0.1 % |
| naca | 6 | 0.1 % |
| element | 6 | 0.1 % |
| nigmatulin | 6 | 0.1 % |
| pumps | 6 | 0.1 % |
| turbulence | 6 | 0.1 % |
| ship | 6 | 0.1 % |
| grid | 5 | 0.1 % |
| heat | 5 | 0.1 % |
| kedrinskii | 5 | 0.1 % |
| piping | 5 | 0.1 % |
| video | 5 | 0.1 % |
| how | 5 | 0.1 % |
| de | 5 | 0.1 % |
| collapse | 5 | 0.1 % |
| unsteady | 5 | 0.1 % |
| flows | 5 | 0.1 % |
| acoustic | 5 | 0.1 % |
| rotating | 5 | 0.1 % |
| ventilated | 5 | 0.1 % |
| velocity | 5 | 0.1 % |
| sizing | 5 | 0.1 % |
| an | 5 | 0.1 % |
| reynolds | 5 | 0.1 % |
| between | 5 | 0.1 % |
| pictures | 5 | 0.1 % |
| - | 5 | 0.1 % |
| modeling | 5 | 0.1 % |
| using | 5 | 0.1 % |
| dynamic | 5 | 0.1 % |
| investigation | 5 | 0.1 % |
| condition | 5 | 0.1 % |
| spectrum | 5 | 0.1 % |
| inception | 5 | 0.1 % |
| super | 4 | 0.1 % |
| experiment | 4 | 0.1 % |
| fluid | 4 | 0.1 % |
| type | 4 | 0.1 % |
| injector | 4 | 0.1 % |
| intake | 4 | 0.1 % |
| laser | 4 | 0.1 % |
| scale | 4 | 0.1 % |
| emission | 4 | 0.1 % |
| oscillation | 4 | 0.1 % |
| & | 4 | 0.1 % |
| liquid | 4 | 0.1 % |
| hydrodynamics | 4 | 0.1 % |
| pan-xiang-wu | 4 | 0.1 % |
| sae | 4 | 0.1 % |
| transfer | 4 | 0.1 % |
| angle | 4 | 0.1 % |
| arndt | 4 | 0.1 % |
| kinnas | 4 | 0.1 % |
| code | 4 | 0.1 % |
| waves | 4 | 0.1 % |
| technology | 4 | 0.1 % |
| steady | 4 | 0.1 % |
| nozzles | 4 | 0.1 % |
| discharge | 4 | 0.1 % |
| .pdf | 4 | 0.1 % |
| two | 4 | 0.1 % |
| diesel | 4 | 0.1 % |
| sheet | 4 | 0.1 % |
| submarine | 4 | 0.1 % |
| limit | 4 | 0.1 % |
| hydrophone | 4 | 0.1 % |
| franc | 4 | 0.1 % |
| drop | 4 | 0.1 % |
| from | 4 | 0.1 % |
| kjeldsen | 4 | 0.1 % |
| material | 4 | 0.1 % |
| rudder | 4 | 0.1 % |
| cluster | 4 | 0.1 % |
| particles | 4 | 0.1 % |
| calculations | 3 | 0 % |
| incipient | 3 | 0 % |
| direction | 3 | 0 % |
| phase | 3 | 0 % |
| helical | 3 | 0 % |
| rate | 3 | 0 % |
| drag | 3 | 0 % |
| explosion | 3 | 0 % |
| empirical | 3 | 0 % |
| series | 3 | 0 % |
| artificial | 3 | 0 % |
| nuclei | 3 | 0 % |
| mass | 3 | 0 % |
| about | 3 | 0 % |
| skew | 3 | 0 % |
| liquids | 3 | 0 % |
| calcs | 3 | 0 % |
| performance | 3 | 0 % |
| thermal | 3 | 0 % |
| cone | 3 | 0 % |
| hull | 3 | 0 % |
| intitle | 3 | 0 % |
| length | 3 | 0 % |
| almost | 3 | 0 % |
| hydrofoils | 3 | 0 % |
| valves | 3 | 0 % |
| molecular | 3 | 0 % |
| seawater | 3 | 0 % |
| rarefactions | 3 | 0 % |
| hydrofoil | 3 | 0 % |
| motion | 3 | 0 % |
| wake | 3 | 0 % |
| inanç | 3 | 0 % |
| theory | 3 | 0 % |
| turbomachinery | 3 | 0 % |
| shape | 3 | 0 % |
| tullis | 3 | 0 % |
| edge | 3 | 0 % |
| force | 3 | 0 % |
| experiments | 3 | 0 % |
| history | 3 | 0 % |
| re-entrant | 3 | 0 % |
| raabe | 3 | 0 % |
| thesis | 3 | 0 % |
| chord | 3 | 0 % |
| mechanism | 3 | 0 % |
| spherical | 3 | 0 % |
| boncinelli | 3 | 0 % |
| problems | 3 | 0 % |
| hypervelocity | 3 | 0 % |
| second | 3 | 0 % |
| modified | 3 | 0 % |
| body | 3 | 0 % |
| work | 3 | 0 % |
| single | 3 | 0 % |
| cloud | 3 | 0 % |
| fourth | 3 | 0 % |
| prediction | 3 | 0 % |
| paolo | 3 | 0 % |
| conclusion | 3 | 0 % |
| temperature | 3 | 0 % |
| weitendorf | 3 | 0 % |
| turbo | 3 | 0 % |
| yuan | 3 | 0 % |
| şenocak | 3 | 0 % |
| computation | 3 | 0 % |
| induced | 3 | 0 % |
| explosive | 3 | 0 % |
| definition | 3 | 0 % |
| takahira | 3 | 0 % |
| instabilities | 3 | 0 % |
| micro | 3 | 0 % |
| supercavity | 3 | 0 % |
| near | 3 | 0 % |
| calculate | 3 | 0 % |
| www.aero.ufl.edu/cfd/ | 3 | 0 % |
| at | 3 | 0 % |
| bursts | 3 | 0 % |
| leakage | 3 | 0 % |
| gl | 2 | 0 % |
| trans | 2 | 0 % |
| martin | 2 | 0 % |
| osborn | 2 | 0 % |
| finite | 2 | 0 % |
| light | 2 | 0 % |
| equilibrium | 2 | 0 % |
| wall | 2 | 0 % |
| 1989 | 2 | 0 % |
| marine | 2 | 0 % |
| procedure | 2 | 0 % |
| various | 2 | 0 % |
| supercavities | 2 | 0 % |
| schaffar | 2 | 0 % |
| recovery | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| plates | 2 | 0 % |
| potential-based | 2 | 0 % |
| pond | 2 | 0 % |
| different | 2 | 0 % |
| computational | 2 | 0 % |
| sweep | 2 | 0 % |
| caracterstics | 2 | 0 % |
| s.w. | 2 | 0 % |
| vortices | 2 | 0 % |
| 1992 | 2 | 0 % |
| weixing | 2 | 0 % |
| perspectives | 2 | 0 % |
| vapor | 2 | 0 % |
| naca0015 | 2 | 0 % |
| spillways | 2 | 0 % |
| local | 2 | 0 % |
| journal | 2 | 0 % |
| institute | 2 | 0 % |
| asymptotic | 2 | 0 % |
| ittc | 2 | 0 % |
| step | 2 | 0 % |
| rayleigh-plesset | 2 | 0 % |
| axial | 2 | 0 % |
| un | 2 | 0 % |
| florence | 2 | 0 % |
| wing | 2 | 0 % |
| misty | 2 | 0 % |
| approximation | 2 | 0 % |
| shen | 2 | 0 % |
| p | 2 | 0 % |
| y | 2 | 0 % |
| sound | 2 | 0 % |
| visualization | 2 | 0 % |
| la | 2 | 0 % |
| alajbegovic | 2 | 0 % |
| cascade | 2 | 0 % |
| astm | 2 | 0 % |
| index | 2 | 0 % |
| intensity | 2 | 0 % |
| pitching | 2 | 0 % |
| stokes | 2 | 0 % |
| semi | 2 | 0 % |
| 232. | 2 | 0 % |
| fin | 2 | 0 % |
| impact | 2 | 0 % |
| asme | 2 | 0 % |
| free | 2 | 0 % |
| theoretical | 2 | 0 % |
| turbines | 2 | 0 % |
| distance | 2 | 0 % |
| bernd | 2 | 0 % |
| that | 2 | 0 % |
| clusters | 2 | 0 % |
| line | 2 | 0 % |
| similarity | 2 | 0 % |
| inducers | 2 | 0 % |
| measurements | 2 | 0 % |
| tokumasu | 2 | 0 % |
| web | 2 | 0 % |
| spectrometer | 2 | 0 % |
| dissolved | 2 | 0 % |
| vessel | 2 | 0 % |
| non | 2 | 0 % |
| fortes | 2 | 0 % |
| s. | 2 | 0 % |
| compressible | 2 | 0 % |
| solutions | 2 | 0 % |
| application | 2 | 0 % |
| determine | 2 | 0 % |
| measure | 2 | 0 % |
| savchenco | 2 | 0 % |
| salvatore | 2 | 0 % |
| turbulent | 2 | 0 % |
| numeca | 2 | 0 % |
| pump.pdf | 2 | 0 % |
| comparison | 2 | 0 % |
| sigma | 2 | 0 % |
| torsion | 2 | 0 % |
| methodology | 2 | 0 % |
| tank | 2 | 0 % |
| lagrangian | 2 | 0 % |
| salt | 2 | 0 % |
| piv | 2 | 0 % |
| ersosion | 2 | 0 % |
| axisymmetrical | 2 | 0 % |
| intense | 2 | 0 % |
| joint-time | 2 | 0 % |
| senocak | 2 | 0 % |
| maximum | 2 | 0 % |
| barnaby | 2 | 0 % |
| bem | 2 | 0 % |
| ae | 2 | 0 % |
| matuska | 2 | 0 % |
| o | 2 | 0 % |
| content | 2 | 0 % |
| d | 2 | 0 % |
| upstream | 2 | 0 % |
| oscillates | 2 | 0 % |
| engineering | 2 | 0 % |
| difference | 2 | 0 % |
| scheme | 2 | 0 % |
| al | 2 | 0 % |
| stage | 2 | 0 % |
| hosangadi | 2 | 0 % |
| section | 2 | 0 % |
| size | 2 | 0 % |
| spray | 2 | 0 % |
| mathematic | 2 | 0 % |
| dr | 2 | 0 % |
| signal | 2 | 0 % |
| a-86 | 2 | 0 % |
| critical | 2 | 0 % |
| et | 2 | 0 % |
| compressibility | 2 | 0 % |
| transient | 2 | 0 % |
| simulations | 2 | 0 % |
| use | 2 | 0 % |
| francis | 2 | 0 % |
| university | 2 | 0 % |
| stoffel | 2 | 0 % |
| backward | 2 | 0 % |
| delale | 2 | 0 % |
| results | 2 | 0 % |
| sharp-edged | 2 | 0 % |
| insean | 2 | 0 % |
| steel | 2 | 0 % |
| g | 2 | 0 % |
| doppler | 2 | 0 % |
| c.a | 2 | 0 % |
| derivation | 2 | 0 % |
| damping | 2 | 0 % |
| escaler | 2 | 0 % |
| tube | 2 | 0 % |
| logvinovich | 2 | 0 % |
| scott | 2 | 0 % |
| 2009 | 2 | 0 % |
| integral | 2 | 0 % |
| jean-pierre | 2 | 0 % |
| correction | 2 | 0 % |
| merkles | 2 | 0 % |
| thrust | 2 | 0 % |
| a. | 2 | 0 % |
| natural | 2 | 0 % |
| generated | 2 | 0 % |
| bubbly | 2 | 0 % |
| govindarajan | 2 | 0 % |
| g134 | 2 | 0 % |
| stinebring | 2 | 0 % |
| inst. | 2 | 0 % |
| extrema | 2 | 0 % |
| ultrasonic | 2 | 0 % |
| 1897 | 2 | 0 % |
| gowing | 2 | 0 % |
| fvm | 2 | 0 % |
| ... | 2 | 0 % |
| stator | 2 | 0 % |
| labview | 2 | 0 % |
| wear | 2 | 0 % |
| parsons | 2 | 0 % |
| luminescence | 2 | 0 % |
| testing | 2 | 0 % |
| phenomena | 2 | 0 % |
| plesset | 2 | 0 % |
| waterjet | 2 | 0 % |
| dimotakis | 2 | 0 % |
| keller | 2 | 0 % |
| simple | 2 | 0 % |
| installation | 2 | 0 % |
| nav. | 2 | 0 % |
| 66 | 2 | 0 % |
| ashvin | 2 | 0 % |
| ultra | 2 | 0 % |
| arch. | 2 | 0 % |
| morten | 2 | 0 % |
| oint | 2 | 0 % |
| nuwc | 2 | 0 % |
| abstract | 2 | 0 % |
| picture | 2 | 0 % |
| towing | 2 | 0 % |
| nscbc | 2 | 0 % |
| 38 | 2 | 0 % |
| structure | 2 | 0 % |
| slender | 2 | 0 % |
| spl | 1 | 0 % |
| addes | 1 | 0 % |
| n. | 1 | 0 % |
| projectile | 1 | 0 % |
| -gas | 1 | 0 % |
| rigid | 1 | 0 % |
| pitting | 1 | 0 % |
| materials | 1 | 0 % |
| mixtures | 1 | 0 % |
| emerson | 1 | 0 % |
| used | 1 | 0 % |
| gravity | 1 | 0 % |
| horn | 1 | 0 % |
| energy | 1 | 0 % |
| steps | 1 | 0 % |
| scaling | 1 | 0 % |
| users | 1 | 0 % |
| cylinder | 1 | 0 % |
| interpolation | 1 | 0 % |
| turning | 1 | 0 % |
| shockwave | 1 | 0 % |
| analyser | 1 | 0 % |
| tailai | 1 | 0 % |
| def | 1 | 0 % |
| hydrofoil.pdf | 1 | 0 % |
| panasonic | 1 | 0 % |
| reduce | 1 | 0 % |
| part | 1 | 0 % |
| figures | 1 | 0 % |
| froude | 1 | 0 % |
| exercise | 1 | 0 % |
| can | 1 | 0 % |
| where | 1 | 0 % |
| rankine | 1 | 0 % |
| prop | 1 | 0 % |
| lab | 1 | 0 % |
| analyzer | 1 | 0 % |
| jonboat | 1 | 0 % |
| coefficients | 1 | 0 % |
| cavitation. | 1 | 0 % |
| rf | 1 | 0 % |
| lindau | 1 | 0 % |
| isl | 1 | 0 % |
| lomax | 1 | 0 % |
| 1999 | 1 | 0 % |
| nucleation | 1 | 0 % |
| spalding | 1 | 0 % |
| hall | 1 | 0 % |
| rotordynamic | 1 | 0 % |
| charactristic | 1 | 0 % |
| singularities | 1 | 0 % |
| runner | 1 | 0 % |
| ccd | 1 | 0 % |
| coutier-delgosha | 1 | 0 % |
| problem | 1 | 0 % |
| aluminum | 1 | 0 % |
| trailing | 1 | 0 % |
| mechanics | 1 | 0 % |
| lagrange | 1 | 0 % |
| means | 1 | 0 % |
| proceedings | 1 | 0 % |
| knapp | 1 | 0 % |
| moving | 1 | 0 % |
| stainless | 1 | 0 % |
| fatigue | 1 | 0 % |
| avoid | 1 | 0 % |
| ductile | 1 | 0 % |
| cauchy | 1 | 0 % |
| karki | 1 | 0 % |
| formulas | 1 | 0 % |
| 26t02.001-a | 1 | 0 % |
| conducting | 1 | 0 % |
| inlet | 1 | 0 % |
| fast | 1 | 0 % |
| kuhn | 1 | 0 % |
| equations | 1 | 0 % |
| laminar | 1 | 0 % |
| mode | 1 | 0 % |
| andrew | 1 | 0 % |
| resonator | 1 | 0 % |
| gate | 1 | 0 % |
| strip | 1 | 0 % |
| formulae | 1 | 0 % |
| presented | 1 | 0 % |
| weber | 1 | 0 % |
| change | 1 | 0 % |
| implicit | 1 | 0 % |
| affect | 1 | 0 % |
| partially | 1 | 0 % |
| henda | 1 | 0 % |
| le-7 | 1 | 0 % |
| hj | 1 | 0 % |
| kavitation | 1 | 0 % |
| density | 1 | 0 % |
| joussellin | 1 | 0 % |
| sensitivity | 1 | 0 % |
| chapman | 1 | 0 % |
| clark | 1 | 0 % |
| turbine.pdf | 1 | 0 % |
| submergence | 1 | 0 % |
| discrete | 1 | 0 % |
| gage | 1 | 0 % |
| computing | 1 | 0 % |
| california | 1 | 0 % |
| 51407 | 1 | 0 % |
| measuring | 1 | 0 % |
| idling | 1 | 0 % |
| flip | 1 | 0 % |
| centerfugal | 1 | 0 % |
| gieseketj@npt.nuwc.navy.mil | 1 | 0 % |
| kijelző | 1 | 0 % |
| ellipsoid | 1 | 0 % |
| reactor | 1 | 0 % |
| 0020 | 1 | 0 % |
| k.kamijo | 1 | 0 % |
| inc. | 1 | 0 % |
| pdfs | 1 | 0 % |
| supersonic | 1 | 0 % |
| facing | 1 | 0 % |
| instability | 1 | 0 % |
| j | 1 | 0 % |
| destabilizes | 1 | 0 % |
| naca0012- | 1 | 0 % |
| pitch | 1 | 0 % |
| plunger | 1 | 0 % |
| shuttle | 1 | 0 % |
| b. | 1 | 0 % |
| crack | 1 | 0 % |
| chaves | 1 | 0 % |
| models | 1 | 0 % |
| reducing | 1 | 0 % |
| propulsors | 1 | 0 % |
| similarities | 1 | 0 % |
| ring | 1 | 0 % |
| parameter | 1 | 0 % |
| york | 1 | 0 % |
| stern | 1 | 0 % |
| creating | 1 | 0 % |
| relation | 1 | 0 % |
| allmaras | 1 | 0 % |
| uncertainty | 1 | 0 % |
| affecting | 1 | 0 % |
| contact | 1 | 0 % |
| rules | 1 | 0 % |
| chyczewski | 1 | 0 % |
| bodies | 1 | 0 % |
| vof | 1 | 0 % |
| convergent-divergent | 1 | 0 % |
| vasin | 1 | 0 % |
| plane | 1 | 0 % |
| fresh | 1 | 0 % |
| meyer | 1 | 0 % |
| a4 | 1 | 0 % |
| point | 1 | 0 % |
| increasing | 1 | 0 % |
| eulerian | 1 | 0 % |
| liquid-gas | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| da | 1 | 0 % |
| montage | 1 | 0 % |
| tr. | 1 | 0 % |
| bar | 1 | 0 % |
| pur | 1 | 0 % |
| ultrasonics | 1 | 0 % |
| regiane | 1 | 0 % |
| jtfa | 1 | 0 % |
| multiblock | 1 | 0 % |
| sump | 1 | 0 % |
| internationa | 1 | 0 % |
| turbomachine | 1 | 0 % |
| distribution | 1 | 0 % |
| related | 1 | 0 % |
| sem | 1 | 0 % |
| low-head | 1 | 0 % |
| savchenko | 1 | 0 % |
| refraction | 1 | 0 % |
| naca0006 | 1 | 0 % |
| vladimir.krasilnikov | 1 | 0 % |
| absorbents | 1 | 0 % |
| billet | 1 | 0 % |
| dimensional | 1 | 0 % |
| orifises | 1 | 0 % |
| meters | 1 | 0 % |
| patella | 1 | 0 % |
| air-water | 1 | 0 % |
| noncircular | 1 | 0 % |
| fluids | 1 | 0 % |
| cavitators | 1 | 0 % |
| prosperetti | 1 | 0 % |
| lecture | 1 | 0 % |
| multi-phase | 1 | 0 % |
| notes | 1 | 0 % |
| pellone | 1 | 0 % |
| cavitator | 1 | 0 % |
| lasers | 1 | 0 % |
| hi | 1 | 0 % |
| containing | 1 | 0 % |
| oti | 1 | 0 % |
| two-phase | 1 | 0 % |
| bladed | 1 | 0 % |
| off | 1 | 0 % |
| matrix | 1 | 0 % |
| restricted | 1 | 0 % |
| similar | 1 | 0 % |
| curvilinear | 1 | 0 % |
| uhlman | 1 | 0 % |
| prandtl | 1 | 0 % |
| blvd | 1 | 0 % |
| helmholtz | 1 | 0 % |
| nswc | 1 | 0 % |
| gindroz | 1 | 0 % |
| circle | 1 | 0 % |
| fluent5 | 1 | 0 % |
| pref | 1 | 0 % |
| rapposelli | 1 | 0 % |
| prentice-hall | 1 | 0 % |
| ” | 1 | 0 % |
| partical | 1 | 0 % |
| propellor | 1 | 0 % |
| emilio | 1 | 0 % |
| ventilation | 1 | 0 % |
| formulation | 1 | 0 % |
| position | 1 | 0 % |
| dr. | 1 | 0 % |
| papers | 1 | 0 % |
| low | 1 | 0 % |
| polymer | 1 | 0 % |
| torpedo | 1 | 0 % |
| surface-piercing | 1 | 0 % |
| under | 1 | 0 % |
| [pdf]tip | 1 | 0 % |
| across | 1 | 0 % |
| 8103 | 1 | 0 % |
| djeridi | 1 | 0 % |
| fluctuation | 1 | 0 % |
| -hitachi | 1 | 0 % |
| nanomizer | 1 | 0 % |
| foil | 1 | 0 % |
| boger | 1 | 0 % |
| 5d | 1 | 0 % |
| attenuation | 1 | 0 % |
| eulerian-lagrangian | 1 | 0 % |
| gaussian | 1 | 0 % |
| property | 1 | 0 % |
| lox | 1 | 0 % |
| transition | 1 | 0 % |
| surge | 1 | 0 % |
| impacts | 1 | 0 % |
| francesco | 1 | 0 % |
| cav2001.com | 1 | 0 % |
| 1. | 1 | 0 % |
| layer | 1 | 0 % |
| secondary | 1 | 0 % |
| pt102-14d | 1 | 0 % |
| committee | 1 | 0 % |
| vulcain | 1 | 0 % |
| bearing | 1 | 0 % |
| residual | 1 | 0 % |
| added | 1 | 0 % |
| a8 | 1 | 0 % |
| solution | 1 | 0 % |
| propulsion | 1 | 0 % |
| maines | 1 | 0 % |
| multiorifice | 1 | 0 % |
| reflecting | 1 | 0 % |
| camera | 1 | 0 % |
| spot | 1 | 0 % |
| hydro | 1 | 0 % |
| 16-006 | 1 | 0 % |
| merkle | 1 | 0 % |
| modele | 1 | 0 % |
| investigations | 1 | 0 % |
| stft | 1 | 0 % |
| atlar | 1 | 0 % |
| structure-born | 1 | 0 % |
| shrinking | 1 | 0 % |
| prabhukumar | 1 | 0 % |
| topolnikov | 1 | 0 % |
| does | 1 | 0 % |
| brennen | 1 | 0 % |
| field | 1 | 0 % |
| maxey | 1 | 0 % |
| velocimetry | 1 | 0 % |
| erosin | 1 | 0 % |
| possessing | 1 | 0 % |
| furukawa | 1 | 0 % |
| bodies. | 1 | 0 % |
| kc | 1 | 0 % |
| dhiman | 1 | 0 % |
| damage | 1 | 0 % |
| degree | 1 | 0 % |
| interaction | 1 | 0 % |
| strategy | 1 | 0 % |
| purpose | 1 | 0 % |
| boundaries. | 1 | 0 % |
| young | 1 | 0 % |
| center | 1 | 0 % |
| basis | 1 | 0 % |
| y.tsujimoto | 1 | 0 % |
| independence | 1 | 0 % |
| inside | 1 | 0 % |
| physical | 1 | 0 % |
| breakdown | 1 | 0 % |
| expansion | 1 | 0 % |
| diatomic | 1 | 0 % |
| space | 1 | 0 % |
| restrictive | 1 | 0 % |
| heating | 1 | 0 % |
| vs | 1 | 0 % |
| initial | 1 | 0 % |
| additives | 1 | 0 % |
| boundaries | 1 | 0 % |
| riley | 1 | 0 % |
| 102 | 1 | 0 % |
| strouhal | 1 | 0 % |
| lavrentyev | 1 | 0 % |
| histogram | 1 | 0 % |
| jacobian | 1 | 0 % |
| 4.0 | 1 | 0 % |
| envelope | 1 | 0 % |
| npsh | 1 | 0 % |
| elastic | 1 | 0 % |
| telephone | 1 | 0 % |
| olofsson | 1 | 0 % |
| j. | 1 | 0 % |
| member | 1 | 0 % |
| mettin | 1 | 0 % |
| 316 | 1 | 0 % |
| spalart | 1 | 0 % |
| delta | 1 | 0 % |
| weisend | 1 | 0 % |
| rev | 1 | 0 % |
| tvc | 1 | 0 % |
| iordansky-kogarko-van | 1 | 0 % |
| geometries | 1 | 0 % |
| ohl | 1 | 0 % |
| cylindrical | 1 | 0 % |
| amplifier | 1 | 0 % |
| rst | 1 | 0 % |
| indeuced | 1 | 0 % |
| divergent | 1 | 0 % |
| zero | 1 | 0 % |
| levels | 1 | 0 % |
| calc | 1 | 0 % |
| tempersature | 1 | 0 % |
| image | 1 | 0 % |
| buoyancy | 1 | 0 % |
| resistance | 1 | 0 % |
| turbopumps | 1 | 0 % |
| jin | 1 | 0 % |
| orlando | 1 | 0 % |
| jw | 1 | 0 % |
| cooling | 1 | 0 % |
| bellmouth | 1 | 0 % |
| review | 1 | 0 % |
| mixture | 1 | 0 % |
| andrea | 1 | 0 % |
| narrow | 1 | 0 % |
| no | 1 | 0 % |
| france | 1 | 0 % |
| gp-mf | 1 | 0 % |
| systems | 1 | 0 % |
| preston | 1 | 0 % |
| user | 1 | 0 % |
| multiphase | 1 | 0 % |
| hollow | 1 | 0 % |
| tropea | 1 | 0 % |
| colonius | 1 | 0 % |
| ionising | 1 | 0 % |
| 0015 | 1 | 0 % |
| scaled-up | 1 | 0 % |
| roe | 1 | 0 % |
| biodiesel | 1 | 0 % |
| filina | 1 | 0 % |
| fcca-ve-50 | 1 | 0 % |
| impeller | 1 | 0 % |
| impellers | 1 | 0 % |
| kunz | 1 | 0 % |
| complex | 1 | 0 % |
| restrict | 1 | 0 % |
| factor | 1 | 0 % |
| disertation | 1 | 0 % |
| valery | 1 | 0 % |
| erosive | 1 | 0 % |
| ordinary | 1 | 0 % |
| discussion | 1 | 0 % |
| tait | 1 | 0 % |
| pattern | 1 | 0 % |
| as | 1 | 0 % |
| jornal | 1 | 0 % |
| 5 | 1 | 0 % |
| | 1 | 0 % |
| has | 1 | 0 % |
| third | 1 | 0 % |
| acrylic | 1 | 0 % |
| ultrasound | 1 | 0 % |
| deutsch | 1 | 0 % |
| 9500 | 1 | 0 % |
| acknowledgement | 1 | 0 % |
| navy | 1 | 0 % |
| break | 1 | 0 % |
| behaviour | 1 | 0 % |
| คือ | 1 | 0 % |
| macarthur | 1 | 0 % |
| hub | 1 | 0 % |
| mechanical | 1 | 0 % |
| versus | 1 | 0 % |
| abs | 1 | 0 % |
| 1997 | 1 | 0 % |
| fortran | 1 | 0 % |
| behind | 1 | 0 % |
| core | 1 | 0 % |
| preamplifier | 1 | 0 % |
| yin | 1 | 0 % |
| charactreistics | 1 | 0 % |
| erosional | 1 | 0 % |
| kind | 1 | 0 % |
| 26th | 1 | 0 % |
| cours | 1 | 0 % |
| sections | 1 | 0 % |
| studie | 1 | 0 % |
| 1976 | 1 | 0 % |
| cryogenic | 1 | 0 % |
| ppt | 1 | 0 % |
| chizelle | 1 | 0 % |
| hole | 1 | 0 % |
| side | 1 | 0 % |
| meter | 1 | 0 % |
| approach | 1 | 0 % |
| multiple | 1 | 0 % |
| cavition | 1 | 0 % |
| technologies | 1 | 0 % |
| chahine | 1 | 0 % |
| smoothing | 1 | 0 % |
| gap | 1 | 0 % |
| cruisers | 1 | 0 % |
| solving | 1 | 0 % |
| new | 1 | 0 % |
| 1996 | 1 | 0 % |
| 25 | 1 | 0 % |
| strategies | 1 | 0 % |
| frigate | 1 | 0 % |
| chimera | 1 | 0 % |
| darmstadt | 1 | 0 % |
| piping? | 1 | 0 % |
| monatomic | 1 | 0 % |
| downstream | 1 | 0 % |
| blake | 1 | 0 % |
| modern | 1 | 0 % |
| alexandra | 1 | 0 % |
| j.p.franc | 1 | 0 % |
| m.yoshida | 1 | 0 % |
| lines | 1 | 0 % |
| lakshminarayana | 1 | 0 % |
| coating | 1 | 0 % |
| reference | 1 | 0 % |
| newton | 1 | 0 % |
| -wind | 1 | 0 % |
| blades | 1 | 0 % |
| cavities | 1 | 0 % |
| principle | 1 | 0 % |
| settings | 1 | 0 % |
| sm | 1 | 0 % |
| gauge | 1 | 0 % |
| water? | 1 | 0 % |
| patankar | 1 | 0 % |
| enhance | 1 | 0 % |
| paradox | 1 | 0 % |
| dampening | 1 | 0 % |
| lubrication | 1 | 0 % |
| christian | 1 | 0 % |
| formation | 1 | 0 % |
| 2008 | 1 | 0 % |
| decomposition | 1 | 0 % |
| open | 1 | 0 % |
| rader | 1 | 0 % |
| clearance | 1 | 0 % |
| contour | 1 | 0 % |
| characterization | 1 | 0 % |
| forms | 1 | 0 % |
| lecture.004 | 1 | 0 % |
| right | 1 | 0 % |
| conclussions | 1 | 0 % |
| specifications | 1 | 0 % |
| lu | 1 | 0 % |
| jules | 1 | 0 % |
| datasheet | 1 | 0 % |
| gosman | 1 | 0 % |
| sapphire | 1 | 0 % |
| lauterborn | 1 | 0 % |
| partial | 1 | 0 % |
| kurtz | 1 | 0 % |
| technology california | 1 | 0 % |
| bearings | 1 | 0 % |
| holes | 1 | 0 % |
| response | 1 | 0 % |
| recommendations | 1 | 0 % |
| because | 1 | 0 % |
| régiane | 1 | 0 % |
| potential | 1 | 0 % |
| gaseous | 1 | 0 % |
| rational | 1 | 0 % |
| experience | 1 | 0 % |
| validation | 1 | 0 % |
| outlet | 1 | 0 % |
| sharp | 1 | 0 % |
| lattice | 1 | 0 % |
| cavitations | 1 | 0 % |
| coupled | 1 | 0 % |
| overset | 1 | 0 % |
| do | 1 | 0 % |
| ships | 1 | 0 % |
| towards | 1 | 0 % |
| propellered | 1 | 0 % |
| homogeneous | 1 | 0 % |
| filter | 1 | 0 % |
| sea | 1 | 0 % |
| paers | 1 | 0 % |
| hiroyuki-takahira | 1 | 0 % |
| outlets | 1 | 0 % |
| chanine | 1 | 0 % |
| craft | 1 | 0 % |
| suitable | 1 | 0 % |
| caviatation | 1 | 0 % |
| burble | 1 | 0 % |
| corner | 1 | 0 % |
| machining | 1 | 0 % |
| neal | 1 | 0 % |
| flux | 1 | 0 % |
| rayleigh | 1 | 0 % |
| 3-d | 1 | 0 % |
| standoff | 1 | 0 % |
| capuani | 1 | 0 % |
| cavitation- | 1 | 0 % |
| hykat | 1 | 0 % |
| diameter | 1 | 0 % |
| 1955 | 1 | 0 % |
| \fluid | 1 | 0 % |
| multi | 1 | 0 % |
| Other words | 69 | 1.7 % |
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