| 1048 different keywords | Search | Percent |
|---|
| cavitation | 284 | 7.3 % |
| of | 172 | 4.4 % |
| orifice | 115 | 2.9 % |
| and | 76 | 1.9 % |
| restriction | 60 | 1.5 % |
| in | 58 | 1.4 % |
| on | 56 | 1.4 % |
| pdf | 46 | 1.1 % |
| flow | 46 | 1.1 % |
| pump | 46 | 1.1 % |
| the | 41 | 1 % |
| propeller | 36 | 0.9 % |
| for | 34 | 0.8 % |
| water | 33 | 0.8 % |
| pressure | 30 | 0.7 % |
| cavitating | 29 | 0.7 % |
| supercavitation | 29 | 0.7 % |
| numerical | 28 | 0.7 % |
| a | 27 | 0.6 % |
| design | 27 | 0.6 % |
| inducer | 26 | 0.6 % |
| bubble | 24 | 0.6 % |
| centrifugal | 24 | 0.6 % |
| vortex | 24 | 0.6 % |
| symposium | 23 | 0.5 % |
| simulation | 22 | 0.5 % |
| unsteady | 20 | 0.5 % |
| analysis | 20 | 0.5 % |
| erosion | 20 | 0.5 % |
| international | 19 | 0.4 % |
| effect | 19 | 0.4 % |
| number | 18 | 0.4 % |
| pumps | 18 | 0.4 % |
| model | 17 | 0.4 % |
| pipe | 15 | 0.3 % |
| to | 15 | 0.3 % |
| valve | 15 | 0.3 % |
| test | 14 | 0.3 % |
| rocket | 14 | 0.3 % |
| supercavitating | 14 | 0.3 % |
| kaplan | 14 | 0.3 % |
| noise | 14 | 0.3 % |
| blade | 13 | 0.3 % |
| with | 13 | 0.3 % |
| at | 13 | 0.3 % |
| scale | 12 | 0.3 % |
| paper | 12 | 0.3 % |
| turbine | 12 | 0.3 % |
| plate | 12 | 0.3 % |
| cavity | 12 | 0.3 % |
| calculation | 12 | 0.3 % |
| experimental | 12 | 0.3 % |
| horn | 11 | 0.2 % |
| bubbles | 11 | 0.2 % |
| distribution | 11 | 0.2 % |
| filetype | 11 | 0.2 % |
| angle | 11 | 0.2 % |
| cav2001 | 11 | 0.2 % |
| orifices | 11 | 0.2 % |
| turbopump | 10 | 0.2 % |
| phase | 10 | 0.2 % |
| boundary | 10 | 0.2 % |
| types | 10 | 0.2 % |
| wave | 10 | 0.2 % |
| ship | 10 | 0.2 % |
| fluent | 10 | 0.2 % |
| rudder | 10 | 0.2 % |
| effects | 10 | 0.2 % |
| dynamics | 9 | 0.2 % |
| mass | 9 | 0.2 % |
| jet | 9 | 0.2 % |
| hydrofoil | 9 | 0.2 % |
| ventilated | 9 | 0.2 % |
| sae | 9 | 0.2 % |
| zero | 9 | 0.2 % |
| modeling | 9 | 0.2 % |
| tunnel | 9 | 0.2 % |
| head | 9 | 0.2 % |
| suction | 9 | 0.2 % |
| method | 9 | 0.2 % |
| by | 8 | 0.2 % |
| study | 8 | 0.2 % |
| technical | 8 | 0.2 % |
| is | 8 | 0.2 % |
| flows | 8 | 0.2 % |
| butterfly | 8 | 0.2 % |
| acoustic | 8 | 0.2 % |
| tip | 8 | 0.2 % |
| an | 8 | 0.2 % |
| yaw | 8 | 0.2 % |
| forms | 8 | 0.2 % |
| forces | 8 | 0.2 % |
| turbo | 8 | 0.2 % |
| cfd | 8 | 0.2 % |
| installation | 8 | 0.2 % |
| frequency | 8 | 0.2 % |
| experiment | 7 | 0.1 % |
| fluid | 7 | 0.1 % |
| surface | 7 | 0.1 % |
| liquid | 7 | 0.1 % |
| length | 7 | 0.1 % |
| template | 7 | 0.1 % |
| added | 7 | 0.1 % |
| velocity | 7 | 0.1 % |
| sizing | 7 | 0.1 % |
| time | 7 | 0.1 % |
| vibration | 7 | 0.1 % |
| tab_hty | 7 | 0.1 % |
| propellers | 7 | 0.1 % |
| modelling | 7 | 0.1 % |
| hydraulic | 7 | 0.1 % |
| joint | 7 | 0.1 % |
| what | 6 | 0.1 % |
| azipod | 6 | 0.1 % |
| jets | 6 | 0.1 % |
| behavior | 6 | 0.1 % |
| coefficient | 6 | 0.1 % |
| stokes | 6 | 0.1 % |
| a.keller | 6 | 0.1 % |
| 3d | 6 | 0.1 % |
| naca | 6 | 0.1 % |
| element | 6 | 0.1 % |
| two | 6 | 0.1 % |
| diesel | 6 | 0.1 % |
| equation | 6 | 0.1 % |
| around | 6 | 0.1 % |
| air | 6 | 0.1 % |
| underwater | 5 | 0.1 % |
| bodies | 5 | 0.1 % |
| cavitator | 5 | 0.1 % |
| hydrofoils | 5 | 0.1 % |
| rotating | 5 | 0.1 % |
| hydrodynamic | 5 | 0.1 % |
| theory | 5 | 0.1 % |
| turbomachinery | 5 | 0.1 % |
| waves | 5 | 0.1 % |
| mechanism | 5 | 0.1 % |
| discharge | 5 | 0.1 % |
| shock | 5 | 0.1 % |
| methods | 5 | 0.1 % |
| cavitaion | 5 | 0.1 % |
| fourth | 5 | 0.1 % |
| cavities | 5 | 0.1 % |
| h. | 5 | 0.1 % |
| prediction | 5 | 0.1 % |
| damping | 5 | 0.1 % |
| investigation | 5 | 0.1 % |
| nozzle | 5 | 0.1 % |
| high | 5 | 0.1 % |
| opening | 4 | 0.1 % |
| energy | 4 | 0.1 % |
| type | 4 | 0.1 % |
| farrell | 4 | 0.1 % |
| series | 4 | 0.1 % |
| journal | 4 | 0.1 % |
| supersonic | 4 | 0.1 % |
| parameter | 4 | 0.1 % |
| multiperforated | 4 | 0.1 % |
| formula | 4 | 0.1 % |
| hull | 4 | 0.1 % |
| restricted | 4 | 0.1 % |
| investigations | 4 | 0.1 % |
| shape | 4 | 0.1 % |
| physical | 4 | 0.1 % |
| comparison | 4 | 0.1 % |
| nozzles | 4 | 0.1 % |
| - | 4 | 0.1 % |
| speed | 4 | 0.1 % |
| impeller | 4 | 0.1 % |
| backflow | 4 | 0.1 % |
| ultrasound | 4 | 0.1 % |
| size | 4 | 0.1 % |
| side | 4 | 0.1 % |
| new | 4 | 0.1 % |
| dynamic | 4 | 0.1 % |
| clearance | 4 | 0.1 % |
| gas | 4 | 0.1 % |
| instabilities | 4 | 0.1 % |
| rarefaction | 4 | 0.1 % |
| condition | 4 | 0.1 % |
| efficiency | 4 | 0.1 % |
| submerged | 4 | 0.1 % |
| inception | 4 | 0.1 % |
| nexearch | 4 | 0.1 % |
| measurement | 3 | 0 % |
| scaling | 3 | 0 % |
| system | 3 | 0 % |
| marine | 3 | 0 % |
| the use | 3 | 0 % |
| yoshinobu | 3 | 0 % |
| eularian | 3 | 0 % |
| different | 3 | 0 % |
| correlation | 3 | 0 % |
| proceedings | 3 | 0 % |
| avoid | 3 | 0 % |
| vortices | 3 | 0 % |
| kedrinskii | 3 | 0 % |
| drag | 3 | 0 % |
| piping | 3 | 0 % |
| density | 3 | 0 % |
| tsujimoto | 3 | 0 % |
| thickness | 3 | 0 % |
| state | 3 | 0 % |
| how | 3 | 0 % |
| oscillations | 3 | 0 % |
| relation | 3 | 0 % |
| collapse | 3 | 0 % |
| shen | 3 | 0 % |
| compounds | 3 | 0 % |
| cone | 3 | 0 % |
| download | 3 | 0 % |
| oxidize | 3 | 0 % |
| impact | 3 | 0 % |
| low | 3 | 0 % |
| naca16 | 3 | 0 % |
| its | 3 | 0 % |
| based | 3 | 0 % |
| inducers | 3 | 0 % |
| motion | 3 | 0 % |
| time-frequency | 3 | 0 % |
| organic | 3 | 0 % |
| compressible | 3 | 0 % |
| interaction | 3 | 0 % |
| are | 3 | 0 % |
| force | 3 | 0 % |
| experiments | 3 | 0 % |
| initial | 3 | 0 % |
| pictures | 3 | 0 % |
| vortexing | 3 | 0 % |
| explosions | 3 | 0 % |
| attack | 3 | 0 % |
| generation | 3 | 0 % |
| tank | 3 | 0 % |
| order | 3 | 0 % |
| apparatus | 3 | 0 % |
| upstream | 3 | 0 % |
| maneuvering | 3 | 0 % |
| hosangadi | 3 | 0 % |
| characteristics | 3 | 0 % |
| m. | 3 | 0 % |
| meter | 3 | 0 % |
| critical | 3 | 0 % |
| cloud | 3 | 0 % |
| prevention | 3 | 0 % |
| downstream | 3 | 0 % |
| use | 3 | 0 % |
| stoffel | 3 | 0 % |
| viscous | 3 | 0 % |
| throttling | 3 | 0 % |
| sheet | 3 | 0 % |
| navier | 3 | 0 % |
| 2 | 3 | 0 % |
| helium | 3 | 0 % |
| g134 | 3 | 0 % |
| cav | 3 | 0 % |
| partial | 3 | 0 % |
| micro | 3 | 0 % |
| dimotakis | 3 | 0 % |
| machinery | 3 | 0 % |
| 2d | 3 | 0 % |
| characteristic | 3 | 0 % |
| kuiper | 3 | 0 % |
| level | 3 | 0 % |
| onset | 3 | 0 % |
| from | 3 | 0 % |
| michel | 3 | 0 % |
| straight | 3 | 0 % |
| caviation | 2 | 0 % |
| load | 2 | 0 % |
| serebryakov | 2 | 0 % |
| calculations | 2 | 0 % |
| 31 | 2 | 0 % |
| figure | 2 | 0 % |
| turning | 2 | 0 % |
| procedure | 2 | 0 % |
| when | 2 | 0 % |
| schaffar | 2 | 0 % |
| supercavities | 2 | 0 % |
| coefficients | 2 | 0 % |
| k | 2 | 0 % |
| 1999 | 2 | 0 % |
| plates | 2 | 0 % |
| circulating | 2 | 0 % |
| microbubble | 2 | 0 % |
| vertical | 2 | 0 % |
| problem | 2 | 0 % |
| mech. | 2 | 0 % |
| produced | 2 | 0 % |
| heat | 2 | 0 % |
| inlet | 2 | 0 % |
| solid | 2 | 0 % |
| equations | 2 | 0 % |
| explosion | 2 | 0 % |
| change | 2 | 0 % |
| kavitation | 2 | 0 % |
| submergence | 2 | 0 % |
| width | 2 | 0 % |
| injector | 2 | 0 % |
| transducers | 2 | 0 % |
| influence | 2 | 0 % |
| intake | 2 | 0 % |
| free-surface | 2 | 0 % |
| 45 | 2 | 0 % |
| pressures | 2 | 0 % |
| inelastic | 2 | 0 % |
| b. | 2 | 0 % |
| ahuja | 2 | 0 % |
| r. | 2 | 0 % |
| bell | 2 | 0 % |
| tunnels | 2 | 0 % |
| direct | 2 | 0 % |
| wing | 2 | 0 % |
| vof | 2 | 0 % |
| breaking | 2 | 0 % |
| oscillation | 2 | 0 % |
| eulerian | 2 | 0 % |
| relations | 2 | 0 % |
| cavitational | 2 | 0 % |
| lohrberg | 2 | 0 % |
| thermal | 2 | 0 % |
| flow | 2 | 0 % |
| due | 2 | 0 % |
| sump | 2 | 0 % |
| 2001 | 2 | 0 % |
| nonlinear | 2 | 0 % |
| improved | 2 | 0 % |
| bodies[a]1997 | 2 | 0 % |
| found | 2 | 0 % |
| quality | 2 | 0 % |
| g. | 2 | 0 % |
| rev. | 2 | 0 % |
| astm | 2 | 0 % |
| multi-phase | 2 | 0 % |
| intensity | 2 | 0 % |
| 567-603. | 2 | 0 % |
| tension | 2 | 0 % |
| ventilation | 2 | 0 % |
| unstable | 2 | 0 % |
| restricting | 2 | 0 % |
| free | 2 | 0 % |
| papers | 2 | 0 % |
| across | 2 | 0 % |
| oil | 2 | 0 % |
| turbines | 2 | 0 % |
| foil | 2 | 0 % |
| empirically | 2 | 0 % |
| missiles | 2 | 0 % |
| meshes | 2 | 0 % |
| propelers | 2 | 0 % |
| b | 2 | 0 % |
| vulcain | 2 | 0 % |
| propulsion | 2 | 0 % |
| radiated | 2 | 0 % |
| lithotripsy | 2 | 0 % |
| wake | 2 | 0 % |
| deformation | 2 | 0 % |
| s. | 2 | 0 % |
| engine | 2 | 0 % |
| diffusion | 2 | 0 % |
| purpose | 2 | 0 % |
| inside | 2 | 0 % |
| between | 2 | 0 % |
| application | 2 | 0 % |
| reboud | 2 | 0 % |
| procedures | 2 | 0 % |
| boundaries | 2 | 0 % |
| caster | 2 | 0 % |
| code | 2 | 0 % |
| j. | 2 | 0 % |
| re-entrant | 2 | 0 % |
| acceptable | 2 | 0 % |
| orifice.pdf | 2 | 0 % |
| geometries | 2 | 0 % |
| fragmentation | 2 | 0 % |
| resistance | 2 | 0 % |
| les | 2 | 0 % |
| thesis | 2 | 0 % |
| zaleski | 2 | 0 % |
| no | 2 | 0 % |
| annu. | 2 | 0 % |
| 1970 | 2 | 0 % |
| injection | 2 | 0 % |
| multiphase | 2 | 0 % |
| lagrangian | 2 | 0 % |
| ludwig | 2 | 0 % |
| senocak | 2 | 0 % |
| roughness | 2 | 0 % |
| scardovelli | 2 | 0 % |
| why | 2 | 0 % |
| entry | 2 | 0 % |
| manual | 2 | 0 % |
| kato | 2 | 0 % |
| axisymmetric | 2 | 0 % |
| modified | 2 | 0 % |
| abs | 2 | 0 % |
| negative | 2 | 0 % |
| tanguay | 2 | 0 % |
| cw | 2 | 0 % |
| separation | 2 | 0 % |
| using | 2 | 0 % |
| hole | 2 | 0 % |
| attc | 2 | 0 % |
| et | 2 | 0 % |
| three | 2 | 0 % |
| collapsing | 2 | 0 % |
| venturi | 2 | 0 % |
| blades | 2 | 0 % |
| arunajatesan | 2 | 0 % |
| rouse | 2 | 0 % |
| results | 2 | 0 % |
| hofmann | 2 | 0 % |
| omega | 2 | 0 % |
| three-dimensional | 2 | 0 % |
| takahashi | 2 | 0 % |
| tube | 2 | 0 % |
| logvinovich | 2 | 0 % |
| generating | 2 | 0 % |
| radial | 2 | 0 % |
| structures | 2 | 0 % |
| schnerr | 2 | 0 % |
| bubbly | 2 | 0 % |
| induced | 2 | 0 % |
| labview | 2 | 0 % |
| testing | 2 | 0 % |
| phenomena | 2 | 0 % |
| plesset | 2 | 0 % |
| potential | 2 | 0 % |
| validation | 2 | 0 % |
| spectrum | 2 | 0 % |
| cavitations | 2 | 0 % |
| minimum | 2 | 0 % |
| v. | 2 | 0 % |
| range | 2 | 0 % |
| drop | 2 | 0 % |
| robert | 2 | 0 % |
| high-speed | 2 | 0 % |
| calculate | 2 | 0 % |
| near | 2 | 0 % |
| hammer | 2 | 0 % |
| 1998 | 2 | 0 % |
| abstract | 2 | 0 % |
| rayleigh | 2 | 0 % |
| cavity-running | 2 | 0 % |
| studies | 2 | 0 % |
| l. | 2 | 0 % |
| diameter | 2 | 0 % |
| interfacial | 2 | 0 % |
| structure | 2 | 0 % |
| piercing | 2 | 0 % |
| placement | 1 | 0 % |
| sodium | 1 | 0 % |
| synchronious | 1 | 0 % |
| hydofoil | 1 | 0 % |
| implementation | 1 | 0 % |
| finite | 1 | 0 % |
| particle | 1 | 0 % |
| gama | 1 | 0 % |
| install | 1 | 0 % |
| reasons | 1 | 0 % |
| pressure-velocity-density | 1 | 0 % |
| aiaa | 1 | 0 % |
| dimensionality | 1 | 0 % |
| windsurf | 1 | 0 % |
| halogen | 1 | 0 % |
| karman | 1 | 0 % |
| materials | 1 | 0 % |
| installazione | 1 | 0 % |
| power-saving | 1 | 0 % |
| equilibrium | 1 | 0 % |
| wall | 1 | 0 % |
| 1989 | 1 | 0 % |
| rule | 1 | 0 % |
| fraction | 1 | 0 % |
| seed | 1 | 0 % |
| ga | 1 | 0 % |
| volvo | 1 | 0 % |
| cover | 1 | 0 % |
| desinent | 1 | 0 % |
| pire | 1 | 0 % |
| tailai | 1 | 0 % |
| g32 | 1 | 0 % |
| reduce | 1 | 0 % |
| closing | 1 | 0 % |
| knudsen | 1 | 0 % |
| plastics | 1 | 0 % |
| various | 1 | 0 % |
| shimomura | 1 | 0 % |
| responsible | 1 | 0 % |
| initiated | 1 | 0 % |
| super | 1 | 0 % |
| part | 1 | 0 % |
| polytropic | 1 | 0 % |
| figures | 1 | 0 % |
| m.1983 | 1 | 0 % |
| 009 | 1 | 0 % |
| star-cd | 1 | 0 % |
| kubota | 1 | 0 % |
| helical | 1 | 0 % |
| sauer | 1 | 0 % |
| recovery | 1 | 0 % |
| nasa | 1 | 0 % |
| http | 1 | 0 % |
| self-oscillating | 1 | 0 % |
| arc | 1 | 0 % |
| navier-stokes | 1 | 0 % |
| transitions | 1 | 0 % |
| yoko | 1 | 0 % |
| re | 1 | 0 % |
| permission | 1 | 0 % |
| computational | 1 | 0 % |
| gates | 1 | 0 % |
| g-factor | 1 | 0 % |
| runner | 1 | 0 % |
| suciu | 1 | 0 % |
| installed | 1 | 0 % |
| attached | 1 | 0 % |
| industrial | 1 | 0 % |
| estimate | 1 | 0 % |
| mechanics | 1 | 0 % |
| trailing | 1 | 0 % |
| knapp | 1 | 0 % |
| caltech | 1 | 0 % |
| volute | 1 | 0 % |
| spilled | 1 | 0 % |
| 2nd | 1 | 0 % |
| grid | 1 | 0 % |
| yakushiji | 1 | 0 % |
| tamura | 1 | 0 % |
| leal | 1 | 0 % |
| eng. | 1 | 0 % |
| karki | 1 | 0 % |
| brass | 1 | 0 % |
| distributing | 1 | 0 % |
| niclas | 1 | 0 % |
| fully-compressible | 1 | 0 % |
| fluctuating | 1 | 0 % |
| nonequilibrium | 1 | 0 % |
| naca66mod | 1 | 0 % |
| numbers | 1 | 0 % |
| examination | 1 | 0 % |
| inner | 1 | 0 % |
| distortion | 1 | 0 % |
| 3th | 1 | 0 % |
| weber | 1 | 0 % |
| steering | 1 | 0 % |
| video | 1 | 0 % |
| ref | 1 | 0 % |
| henda | 1 | 0 % |
| spillways | 1 | 0 % |
| //cav2001.library.caltech.edu/ | 1 | 0 % |
| i. | 1 | 0 % |
| conditions | 1 | 0 % |
| source | 1 | 0 % |
| wildt | 1 | 0 % |
| front | 1 | 0 % |
| chareteristic | 1 | 0 % |
| wier | 1 | 0 % |
| spectra | 1 | 0 % |
| ratio | 1 | 0 % |
| françis | 1 | 0 % |
| akinori | 1 | 0 % |
| lynn | 1 | 0 % |
| facing | 1 | 0 % |
| hysteresis | 1 | 0 % |
| ship.pdf | 1 | 0 % |
| 0012 | 1 | 0 % |
| artificial | 1 | 0 % |
| 1 | 1 | 0 % |
| step | 1 | 0 % |
| mesh | 1 | 0 % |
| szeri | 1 | 0 % |
| mcnown | 1 | 0 % |
| brest | 1 | 0 % |
| nucleating | 1 | 0 % |
| rayleigh-plesset | 1 | 0 % |
| stress | 1 | 0 % |
| propulsors | 1 | 0 % |
| axial | 1 | 0 % |
| de | 1 | 0 % |
| entrant | 1 | 0 % |
| florence | 1 | 0 % |
| engines | 1 | 0 % |
| liquids | 1 | 0 % |
| j.fluids | 1 | 0 % |
| azimuthal | 1 | 0 % |
| interference | 1 | 0 % |
| elbow | 1 | 0 % |
| contact | 1 | 0 % |
| boiling | 1 | 0 % |
| should | 1 | 0 % |
| pr. | 1 | 0 % |
| emission | 1 | 0 % |
| radius | 1 | 0 % |
| fresh | 1 | 0 % |
| von | 1 | 0 % |
| speeds | 1 | 0 % |
| performance | 1 | 0 % |
| restiction | 1 | 0 % |
| georges | 1 | 0 % |
| cartesian | 1 | 0 % |
| loads | 1 | 0 % |
| 2010-06-10t08 | 1 | 0 % |
| dimensions | 1 | 0 % |
| & | 1 | 0 % |
| mention | 1 | 0 % |
| [overview | 1 | 0 % |
| required | 1 | 0 % |
| bulb | 1 | 0 % |
| sound | 1 | 0 % |
| deep | 1 | 0 % |
| g.v. | 1 | 0 % |
| errosion | 1 | 0 % |
| explicit | 1 | 0 % |
| 1993 | 1 | 0 % |
| injectors | 1 | 0 % |
| regression | 1 | 0 % |
| soyama | 1 | 0 % |
| turbomachine | 1 | 0 % |
| twin | 1 | 0 % |
| sem | 1 | 0 % |
| self-pressurization | 1 | 0 % |
| w | 1 | 0 % |
| groove | 1 | 0 % |
| over | 1 | 0 % |
| inducers? | 1 | 0 % |
| 1952 | 1 | 0 % |
| denshi | 1 | 0 % |
| visualization | 1 | 0 % |
| panel | 1 | 0 % |
| seo | 1 | 0 % |
| epshtein | 1 | 0 % |
| independent | 1 | 0 % |
| suprercavitation | 1 | 0 % |
| delannoy | 1 | 0 % |
| derivative | 1 | 0 % |
| cascade | 1 | 0 % |
| [pdf] | 1 | 0 % |
| lecture | 1 | 0 % |
| pasadena | 1 | 0 % |
| oscillating | 1 | 0 % |
| phases | 1 | 0 % |
| resonant | 1 | 0 % |
| dammage | 1 | 0 % |
| law | 1 | 0 % |
| modelingem | 1 | 0 % |
| oti | 1 | 0 % |
| pitching | 1 | 0 % |
| valves | 1 | 0 % |
| balde | 1 | 0 % |
| circle | 1 | 0 % |
| displacement | 1 | 0 % |
| 7th | 1 | 0 % |
| c | 1 | 0 % |
| formulation | 1 | 0 % |
| optimization | 1 | 0 % |
| position | 1 | 0 % |
| dr. | 1 | 0 % |
| same | 1 | 0 % |
| planing | 1 | 0 % |
| drain | 1 | 0 % |
| deal | 1 | 0 % |
| gh | 1 | 0 % |
| apl | 1 | 0 % |
| chavez | 1 | 0 % |
| polymere | 1 | 0 % |
| through | 1 | 0 % |
| sixth | 1 | 0 % |
| djeridi | 1 | 0 % |
| ballistics | 1 | 0 % |
| fluctuation | 1 | 0 % |
| 5d | 1 | 0 % |
| distance | 1 | 0 % |
| oxidation | 1 | 0 % |
| 7 | 1 | 0 % |
| colussi | 1 | 0 % |
| st.johns | 1 | 0 % |
| that | 1 | 0 % |
| hiroharu | 1 | 0 % |
| obermeier | 1 | 0 % |
| attenuation | 1 | 0 % |
| brix | 1 | 0 % |
| differential | 1 | 0 % |
| loading | 1 | 0 % |
| michurinski | 1 | 0 % |
| similarity | 1 | 0 % |
| mathematica | 1 | 0 % |
| surge | 1 | 0 % |
| quasi-three-dimensional | 1 | 0 % |
| developed | 1 | 0 % |
| comparisons | 1 | 0 % |
| layer | 1 | 0 % |
| optimum | 1 | 0 % |
| applied | 1 | 0 % |
| ofsystems | 1 | 0 % |
| measurements | 1 | 0 % |
| ballast | 1 | 0 % |
| 225 | 1 | 0 % |
| bearing | 1 | 0 % |
| codes | 1 | 0 % |
| excise | 1 | 0 % |
| channel | 1 | 0 % |
| spectrometer | 1 | 0 % |
| transfer | 1 | 0 % |
| real | 1 | 0 % |
| 22nd | 1 | 0 % |
| device | 1 | 0 % |
| spot | 1 | 0 % |
| large | 1 | 0 % |
| toxicity | 1 | 0 % |
| equation source | 1 | 0 % |
| witnessing | 1 | 0 % |
| david | 1 | 0 % |
| given | 1 | 0 % |
| merkle | 1 | 0 % |
| dissipation | 1 | 0 % |
| l.a. | 1 | 0 % |
| arndt | 1 | 0 % |
| missile | 1 | 0 % |
| th | 1 | 0 % |
| inanç | 1 | 0 % |
| er | 1 | 0 % |
| dtmb_1951 | 1 | 0 % |
| jump | 1 | 0 % |
| reynolds | 1 | 0 % |
| furukawa | 1 | 0 % |
| coorection | 1 | 0 % |
| wilson | 1 | 0 % |
| damage | 1 | 0 % |
| wang | 1 | 0 % |
| degree | 1 | 0 % |
| certificate | 1 | 0 % |
| research | 1 | 0 % |
| equivalent | 1 | 0 % |
| l.g. | 1 | 0 % |
| current | 1 | 0 % |
| tullis | 1 | 0 % |
| intakes | 1 | 0 % |
| edge | 1 | 0 % |
| aisi1015 | 1 | 0 % |
| working | 1 | 0 % |
| laws | 1 | 0 % |
| a=0.8 | 1 | 0 % |
| l | 1 | 0 % |
| videos | 1 | 0 % |
| heating | 1 | 0 % |
| measure | 1 | 0 % |
| cleaning | 1 | 0 % |
| sensitive | 1 | 0 % |
| vs | 1 | 0 % |
| parallel | 1 | 0 % |
| 16b | 1 | 0 % |
| strouhal | 1 | 0 % |
| 02 | 1 | 0 % |
| aluminium | 1 | 0 % |
| 16 | 1 | 0 % |
| central | 1 | 0 % |
| 8th | 1 | 0 % |
| vector | 1 | 0 % |
| olofsson | 1 | 0 % |
| history | 1 | 0 % |
| aft | 1 | 0 % |
| turbulent | 1 | 0 % |
| r.daily | 1 | 0 % |
| numeca | 1 | 0 % |
| pump.pdf | 1 | 0 % |
| chamber | 1 | 0 % |
| reduction | 1 | 0 % |
| stiffness | 1 | 0 % |
| … | 1 | 0 % |
| burgess | 1 | 0 % |
| dome | 1 | 0 % |
| doctoral | 1 | 0 % |
| tvc | 1 | 0 % |
| vladimir | 1 | 0 % |
| cylindrical | 1 | 0 % |
| steady | 1 | 0 % |
| influenced | 1 | 0 % |
| all | 1 | 0 % |
| sumps | 1 | 0 % |
| sigma | 1 | 0 % |
| rayleigh-plasset | 1 | 0 % |
| dispersion | 1 | 0 % |
| submersible | 1 | 0 % |
| hybrid | 1 | 0 % |
| -optimization | 1 | 0 % |
| fft | 1 | 0 % |
| turbopumps | 1 | 0 % |
| stability | 1 | 0 % |
| jin | 1 | 0 % |
| azipods | 1 | 0 % |
| oifice | 1 | 0 % |
| luminiscence | 1 | 0 % |
| systems | 1 | 0 % |
| vacuum | 1 | 0 % |
| navyfilm | 1 | 0 % |
| wall-attachment | 1 | 0 % |
| manoeuver | 1 | 0 % |
| diagram | 1 | 0 % |
| data | 1 | 0 % |
| capturing | 1 | 0 % |
| coupling | 1 | 0 % |
| casing | 1 | 0 % |
| kunz | 1 | 0 % |
| rarefraction | 1 | 0 % |
| factor | 1 | 0 % |
| after | 1 | 0 % |
| naca0009 | 1 | 0 % |
| get | 1 | 0 % |
| erosive | 1 | 0 % |
| control | 1 | 0 % |
| investigative | 1 | 0 % |
| manoeuvring | 1 | 0 % |
| szantyr | 1 | 0 % |
| bem | 1 | 0 % |
| back | 1 | 0 % |
| tait | 1 | 0 % |
| izentropic | 1 | 0 % |
| yoichiro | 1 | 0 % |
| spillway | 1 | 0 % |
| relaxation | 1 | 0 % |
| o | 1 | 0 % |
| pits | 1 | 0 % |
| determination | 1 | 0 % |
| problems | 1 | 0 % |
| fingers | 1 | 0 % |
| behaviour | 1 | 0 % |
| second | 1 | 0 % |
| applications | 1 | 0 % |
| difference | 1 | 0 % |
| 115 | 1 | 0 % |
| designer | 1 | 0 % |
| japikse] | 1 | 0 % |
| b-ratio | 1 | 0 % |
| perpectives | 1 | 0 % |
| penta | 1 | 0 % |
| runga | 1 | 0 % |
| flowing | 1 | 0 % |
| catech | 1 | 0 % |
| rarefication | 1 | 0 % |
| must | 1 | 0 % |
| transport | 1 | 0 % |
| sphere | 1 | 0 % |
| bottle | 1 | 0 % |
| edged | 1 | 0 % |
| ln2 | 1 | 0 % |
| physics | 1 | 0 % |
| body | 1 | 0 % |
| swirl | 1 | 0 % |
| sections | 1 | 0 % |
| below | 1 | 0 % |
| cryogenic | 1 | 0 % |
| japikse | 1 | 0 % |
| proc. | 1 | 0 % |
| during | 1 | 0 % |
| edges | 1 | 0 % |
| % | 1 | 0 % |
| lh2 | 1 | 0 % |
| approach | 1 | 0 % |
| appendage | 1 | 0 % |
| cumulative | 1 | 0 % |
| reichardt | 1 | 0 % |
| jet. | 1 | 0 % |
| spt | 1 | 0 % |
| / | 1 | 0 % |
| chahine | 1 | 0 % |
| gap | 1 | 0 % |
| kp | 1 | 0 % |
| solving | 1 | 0 % |
| matsumoto | 1 | 0 % |
| compressibility | 1 | 0 % |
| acting | 1 | 0 % |
| bernoullis | 1 | 0 % |
| designs | 1 | 0 % |
| reynolds-averaged | 1 | 0 % |
| lerbs | 1 | 0 % |
| csd | 1 | 0 % |
| iahr | 1 | 0 % |
| pfleiderer | 1 | 0 % |
| toa | 1 | 0 % |
| j.s. | 1 | 0 % |
| transient | 1 | 0 % |
| pdf.prevention | 1 | 0 % |
| resriction | 1 | 0 % |
| .pdf | 1 | 0 % |
| reference | 1 | 0 % |
| 16c | 1 | 0 % |
| francis | 1 | 0 % |
| orrifice | 1 | 0 % |
| charateristics | 1 | 0 % |
| university | 1 | 0 % |
| 54z | 1 | 0 % |
| volume | 1 | 0 % |
| piezoelektrische | 1 | 0 % |
| temporal | 1 | 0 % |
| higher | 1 | 0 % |
| orifce | 1 | 0 % |
| gauge | 1 | 0 % |
| tests | 1 | 0 % |
| turbulence | 1 | 0 % |
| patankar | 1 | 0 % |
| xviii | 1 | 0 % |
| compare | 1 | 0 % |
| mathematical | 1 | 0 % |
| kutta | 1 | 0 % |
| – | 1 | 0 % |
| steel | 1 | 0 % |
| k-194 | 1 | 0 % |
| conclusion | 1 | 0 % |
| burrill | 1 | 0 % |
| lamp | 1 | 0 % |
| wide | 1 | 0 % |
| temperature | 1 | 0 % |
| basics | 1 | 0 % |
| curvature | 1 | 0 % |
| thermodynamics | 1 | 0 % |
| derivation | 1 | 0 % |
| friedrichs | 1 | 0 % |
| orfices | 1 | 0 % |
| inverse | 1 | 0 % |
| geometric | 1 | 0 % |
| theory. | 1 | 0 % |
| area | 1 | 0 % |
| void | 1 | 0 % |
| aerodynamic | 1 | 0 % |
| www.flow | 1 | 0 % |
| scott | 1 | 0 % |
| supercavitation-problems | 1 | 0 % |
| throgh | 1 | 0 % |
| bucket.pdf | 1 | 0 % |
| integral | 1 | 0 % |
| shyy | 1 | 0 % |
| occurrence | 1 | 0 % |
| japan | 1 | 0 % |
| crash | 1 | 0 % |
| profile | 1 | 0 % |
| yuan | 1 | 0 % |
| holder | 1 | 0 % |
| points | 1 | 0 % |
| a. | 1 | 0 % |
| 1990 | 1 | 0 % |
| govindarajan | 1 | 0 % |
| amd | 1 | 0 % |
| pot | 1 | 0 % |
| typical | 1 | 0 % |
| unstructured | 1 | 0 % |
| şenocak | 1 | 0 % |
| computation | 1 | 0 % |
| vane | 1 | 0 % |
| ryo | 1 | 0 % |
| dci | 1 | 0 % |
| istruzioni | 1 | 0 % |
| yuya | 1 | 0 % |
| bubbler | 1 | 0 % |
| flange | 1 | 0 % |
| s | 1 | 0 % |
| stock | 1 | 0 % |
| yi | 1 | 0 % |
| definition | 1 | 0 % |
| disappearing | 1 | 0 % |
| flux-splitting | 1 | 0 % |
| yamaguchi. | 1 | 0 % |
| luminescence | 1 | 0 % |
| hydrophone | 1 | 0 % |
| coordinates | 1 | 0 % |
| waterjet | 1 | 0 % |
| caltch | 1 | 0 % |
| sharp | 1 | 0 % |
| mixing | 1 | 0 % |
| phd | 1 | 0 % |
| keller | 1 | 0 % |
| kawanami | 1 | 0 % |
| wine | 1 | 0 % |
| foiling | 1 | 0 % |
| transformer | 1 | 0 % |
| simple | 1 | 0 % |
| supercavity | 1 | 0 % |
| flow—a | 1 | 0 % |
| ships | 1 | 0 % |
| homogeneous | 1 | 0 % |
| kjeldsen | 1 | 0 % |
| sea | 1 | 0 % |
| 66 | 1 | 0 % |
| morten | 1 | 0 % |
| lifting | 1 | 0 % |
| caviatation | 1 | 0 % |
| pumped | 1 | 0 % |
| bubble? | 1 | 0 % |
| vehicles | 1 | 0 % |
| xtm-190 | 1 | 0 % |
| decrease | 1 | 0 % |
| blue | 1 | 0 % |
| f. | 1 | 0 % |
| cavitation.pdf | 1 | 0 % |
| pps | 1 | 0 % |
| leakage | 1 | 0 % |
| action | 1 | 0 % |
| kueny | 1 | 0 % |
| multi | 1 | 0 % |
| prinnciple | 1 | 0 % |
| ideal | 1 | 0 % |
| Other words | 48 | 1.2 % |
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