| 1336 different keywords | Search | Percent |
|---|
| cavitation | 575 | 9.9 % |
| of | 153 | 2.6 % |
| pdf | 148 | 2.5 % |
| pump | 136 | 2.3 % |
| propeller | 100 | 1.7 % |
| in | 92 | 1.5 % |
| orifice | 84 | 1.4 % |
| and | 59 | 1 % |
| centrifugal | 59 | 1 % |
| vortex | 58 | 0.9 % |
| flow | 57 | 0.9 % |
| bubble | 54 | 0.9 % |
| water | 51 | 0.8 % |
| restriction | 48 | 0.8 % |
| pressure | 47 | 0.8 % |
| on | 46 | 0.7 % |
| fluent | 44 | 0.7 % |
| filetype | 43 | 0.7 % |
| cavitating | 37 | 0.6 % |
| supercavitation | 36 | 0.6 % |
| a | 33 | 0.5 % |
| propellers | 33 | 0.5 % |
| equation | 32 | 0.5 % |
| numerical | 31 | 0.5 % |
| turbine | 31 | 0.5 % |
| pumps | 31 | 0.5 % |
| the | 31 | 0.5 % |
| hydrofoil | 30 | 0.5 % |
| design | 30 | 0.5 % |
| nexearch | 30 | 0.5 % |
| noise | 30 | 0.5 % |
| analysis | 28 | 0.4 % |
| simulation | 28 | 0.4 % |
| for | 27 | 0.4 % |
| blade | 26 | 0.4 % |
| number | 24 | 0.4 % |
| surface | 24 | 0.4 % |
| impeller | 24 | 0.4 % |
| kaplan | 24 | 0.4 % |
| bubbles | 23 | 0.3 % |
| jet | 23 | 0.3 % |
| cavity | 23 | 0.3 % |
| model | 22 | 0.3 % |
| erosion | 21 | 0.3 % |
| naca | 21 | 0.3 % |
| ship | 21 | 0.3 % |
| suction | 20 | 0.3 % |
| effect | 19 | 0.3 % |
| video | 18 | 0.3 % |
| hydrodynamic | 18 | 0.3 % |
| fluid | 17 | 0.2 % |
| symposium | 17 | 0.2 % |
| laser | 17 | 0.2 % |
| tunnel | 17 | 0.2 % |
| cfd | 17 | 0.2 % |
| effects | 17 | 0.2 % |
| piercing | 17 | 0.2 % |
| distribution | 16 | 0.2 % |
| flows | 16 | 0.2 % |
| tip | 16 | 0.2 % |
| supercavitating | 16 | 0.2 % |
| method | 16 | 0.2 % |
| butterfly | 15 | 0.2 % |
| pictures | 15 | 0.2 % |
| inducer | 15 | 0.2 % |
| rudder | 15 | 0.2 % |
| azipod | 14 | 0.2 % |
| velocity | 14 | 0.2 % |
| frequency | 14 | 0.2 % |
| length | 13 | 0.2 % |
| foil | 13 | 0.2 % |
| to | 13 | 0.2 % |
| dynamics | 12 | 0.2 % |
| test | 12 | 0.2 % |
| liquid | 12 | 0.2 % |
| boundary | 12 | 0.2 % |
| time | 12 | 0.2 % |
| valve | 12 | 0.2 % |
| inception | 12 | 0.2 % |
| intake | 11 | 0.1 % |
| thesis | 11 | 0.1 % |
| modeling | 11 | 0.1 % |
| plate | 11 | 0.1 % |
| characteristics | 11 | 0.1 % |
| orifices | 11 | 0.1 % |
| nozzle | 11 | 0.1 % |
| rayleigh | 11 | 0.1 % |
| turbopump | 10 | 0.1 % |
| study | 10 | 0.1 % |
| photo | 10 | 0.1 % |
| phenomenon | 10 | 0.1 % |
| multiphase | 10 | 0.1 % |
| vibration | 10 | 0.1 % |
| hydraulic | 10 | 0.1 % |
| joint | 10 | 0.1 % |
| underwater | 9 | 0.1 % |
| phase | 9 | 0.1 % |
| by | 9 | 0.1 % |
| how | 9 | 0.1 % |
| scale | 9 | 0.1 % |
| & | 9 | 0.1 % |
| coefficient | 9 | 0.1 % |
| stokes | 9 | 0.1 % |
| off | 9 | 0.1 % |
| atlar | 9 | 0.1 % |
| shape | 9 | 0.1 % |
| cav2001 | 9 | 0.1 % |
| 3d | 9 | 0.1 % |
| 16 | 9 | 0.1 % |
| speed | 9 | 0.1 % |
| spillway | 9 | 0.1 % |
| international | 9 | 0.1 % |
| break | 9 | 0.1 % |
| wave | 9 | 0.1 % |
| size | 9 | 0.1 % |
| two | 9 | 0.1 % |
| calculation | 9 | 0.1 % |
| submerged | 9 | 0.1 % |
| super | 8 | 0.1 % |
| axial | 8 | 0.1 % |
| collapse | 8 | 0.1 % |
| unsteady | 8 | 0.1 % |
| rocket | 8 | 0.1 % |
| damage | 8 | 0.1 % |
| edge | 8 | 0.1 % |
| npsh | 8 | 0.1 % |
| tait | 8 | 0.1 % |
| konno | 8 | 0.1 % |
| element | 8 | 0.1 % |
| venturi | 8 | 0.1 % |
| airfoil | 8 | 0.1 % |
| plesset | 8 | 0.1 % |
| horn | 7 | 0.1 % |
| experiment | 7 | 0.1 % |
| drag | 7 | 0.1 % |
| performance | 7 | 0.1 % |
| savchenko | 7 | 0.1 % |
| propellor | 7 | 0.1 % |
| types | 7 | 0.1 % |
| tank | 7 | 0.1 % |
| prediction | 7 | 0.1 % |
| modelling | 7 | 0.1 % |
| spectrum | 7 | 0.1 % |
| picture | 7 | 0.1 % |
| jets | 6 | 0.1 % |
| grid | 6 | 0.1 % |
| solid | 6 | 0.1 % |
| equations | 6 | 0.1 % |
| partially | 6 | 0.1 % |
| lift | 6 | 0.1 % |
| tsujimoto | 6 | 0.1 % |
| models | 6 | 0.1 % |
| thermal | 6 | 0.1 % |
| 2001 | 6 | 0.1 % |
| cavitator | 6 | 0.1 % |
| free | 6 | 0.1 % |
| similarity | 6 | 0.1 % |
| angle | 6 | 0.1 % |
| an | 6 | 0.1 % |
| history | 6 | 0.1 % |
| injection | 6 | 0.1 % |
| using | 6 | 0.1 % |
| chahine | 6 | 0.1 % |
| backward | 6 | 0.1 % |
| turbulence | 6 | 0.1 % |
| dynamic | 6 | 0.1 % |
| micro | 6 | 0.1 % |
| supercavity | 6 | 0.1 % |
| fig | 6 | 0.1 % |
| emissions | 5 | 0 % |
| kubota | 5 | 0 % |
| navier-stokes | 5 | 0 % |
| mass | 5 | 0 % |
| objects | 5 | 0 % |
| georges | 5 | 0 % |
| introduction | 5 | 0 % |
| hydrodynamics | 5 | 0 % |
| turbines | 5 | 0 % |
| ventilated | 5 | 0 % |
| time-frequency | 5 | 0 % |
| hydro | 5 | 0 % |
| between | 5 | 0 % |
| steady | 5 | 0 % |
| 2000 | 5 | 0 % |
| senocak | 5 | 0 % |
| spherical | 5 | 0 % |
| turbin | 5 | 0 % |
| specific | 5 | 0 % |
| cryogenic | 5 | 0 % |
| turbomachines | 5 | 0 % |
| methods | 5 | 0 % |
| integral | 5 | 0 % |
| sheet | 5 | 0 % |
| head | 5 | 0 % |
| characteristic | 5 | 0 % |
| ships | 5 | 0 % |
| adaptable | 5 | 0 % |
| abstract | 5 | 0 % |
| photos | 5 | 0 % |
| at | 5 | 0 % |
| diameter | 5 | 0 % |
| author | 4 | 0 % |
| yuriy | 4 | 0 % |
| non-equilibrium | 4 | 0 % |
| munition | 4 | 0 % |
| type | 4 | 0 % |
| incompressible | 4 | 0 % |
| inlet | 4 | 0 % |
| injector | 4 | 0 % |
| series | 4 | 0 % |
| journal | 4 | 0 % |
| pipe | 4 | 0 % |
| about | 4 | 0 % |
| ahuja | 4 | 0 % |
| bell | 4 | 0 % |
| vof | 4 | 0 % |
| 4412 | 4 | 0 % |
| oscillation | 4 | 0 % |
| formed | 4 | 0 % |
| sump | 4 | 0 % |
| paper | 4 | 0 % |
| acoustic | 4 | 0 % |
| webkr | 4 | 0 % |
| parameters | 4 | 0 % |
| impact | 4 | 0 % |
| surface-piercing | 4 | 0 % |
| through | 4 | 0 % |
| undersea | 4 | 0 % |
| observations | 4 | 0 % |
| merkle | 4 | 0 % |
| arndt | 4 | 0 % |
| or | 4 | 0 % |
| theory | 4 | 0 % |
| reynolds | 4 | 0 % |
| are | 4 | 0 % |
| - | 4 | 0 % |
| roughness | 4 | 0 % |
| mechanism | 4 | 0 % |
| maximum | 4 | 0 % |
| problems | 4 | 0 % |
| difference | 4 | 0 % |
| body | 4 | 0 % |
| single | 4 | 0 % |
| k-omega | 4 | 0 % |
| use | 4 | 0 % |
| volume | 4 | 0 % |
| h. | 4 | 0 % |
| diesel | 4 | 0 % |
| properties | 4 | 0 % |
| gas | 4 | 0 % |
| shyy | 4 | 0 % |
| turbo | 4 | 0 % |
| yuan | 4 | 0 % |
| submarine | 4 | 0 % |
| induced | 4 | 0 % |
| instabilities | 4 | 0 % |
| nitrogen | 4 | 0 % |
| luminescence | 4 | 0 % |
| hydrophone | 4 | 0 % |
| around | 4 | 0 % |
| 2d | 4 | 0 % |
| from | 4 | 0 % |
| site | 4 | 0 % |
| high-speed | 4 | 0 % |
| leading | 4 | 0 % |
| high | 4 | 0 % |
| experimental | 4 | 0 % |
| towing | 4 | 0 % |
| air | 4 | 0 % |
| what | 3 | 0 % |
| calculations | 3 | 0 % |
| measurement | 3 | 0 % |
| wall | 3 | 0 % |
| marine | 3 | 0 % |
| curves | 3 | 0 % |
| rankine | 3 | 0 % |
| lindau | 3 | 0 % |
| hydrocode | 3 | 0 % |
| runner | 3 | 0 % |
| trailing | 3 | 0 % |
| moving | 3 | 0 % |
| caltech | 3 | 0 % |
| volute | 3 | 0 % |
| ductile | 3 | 0 % |
| heat | 3 | 0 % |
| gp-mf-552 | 3 | 0 % |
| explosion | 3 | 0 % |
| piping | 3 | 0 % |
| kavitation | 3 | 0 % |
| case | 3 | 0 % |
| ratio | 3 | 0 % |
| ittc | 3 | 0 % |
| rayleigh-plesset | 3 | 0 % |
| nd | 3 | 0 % |
| relation | 3 | 0 % |
| liquids | 3 | 0 % |
| y | 3 | 0 % |
| formula | 3 | 0 % |
| sound | 3 | 0 % |
| cone | 3 | 0 % |
| small | 3 | 0 % |
| fluids | 3 | 0 % |
| cascade | 3 | 0 % |
| sonic | 3 | 0 % |
| index | 3 | 0 % |
| calculating | 3 | 0 % |
| pellone | 3 | 0 % |
| two-phase | 3 | 0 % |
| antony | 3 | 0 % |
| skewed | 3 | 0 % |
| unstable | 3 | 0 % |
| 1944 | 3 | 0 % |
| wedge | 3 | 0 % |
| papers | 3 | 0 % |
| low | 3 | 0 % |
| yag | 3 | 0 % |
| surge | 3 | 0 % |
| inducers | 3 | 0 % |
| atomization | 3 | 0 % |
| with | 3 | 0 % |
| measurements | 3 | 0 % |
| function | 3 | 0 % |
| bearing | 3 | 0 % |
| added | 3 | 0 % |
| 1994 | 3 | 0 % |
| pearson | 3 | 0 % |
| 16-006 | 3 | 0 % |
| process | 3 | 0 % |
| kinnas | 3 | 0 % |
| engine | 3 | 0 % |
| turbomachinery | 3 | 0 % |
| compressible | 3 | 0 % |
| reboud | 3 | 0 % |
| videos | 3 | 0 % |
| conical | 3 | 0 % |
| power | 3 | 0 % |
| reduction | 3 | 0 % |
| technology | 3 | 0 % |
| amplifier | 3 | 0 % |
| ando | 3 | 0 % |
| mixture | 3 | 0 % |
| order | 3 | 0 % |
| diagram | 3 | 0 % |
| fruman | 3 | 0 % |
| ultrasound | 3 | 0 % |
| discharge | 3 | 0 % |
| second | 3 | 0 % |
| negative | 3 | 0 % |
| stage | 3 | 0 % |
| section | 3 | 0 % |
| hosangadi | 3 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 3 | 0 % |
| during | 3 | 0 % |
| approach | 3 | 0 % |
| cloud | 3 | 0 % |
| images | 3 | 0 % |
| .pdf | 3 | 0 % |
| francis | 3 | 0 % |
| blades | 3 | 0 % |
| steel | 3 | 0 % |
| christian | 3 | 0 % |
| temperature | 3 | 0 % |
| damping | 3 | 0 % |
| cutting | 3 | 0 % |
| forces | 3 | 0 % |
| weitendorf | 3 | 0 % |
| thruster | 3 | 0 % |
| a. | 3 | 0 % |
| computation | 3 | 0 % |
| vane | 3 | 0 % |
| s | 3 | 0 % |
| bearings | 3 | 0 % |
| rarefaction | 3 | 0 % |
| sonochemistry | 3 | 0 % |
| testing | 3 | 0 % |
| phenomena | 3 | 0 % |
| validation | 3 | 0 % |
| waterjet | 3 | 0 % |
| loss | 3 | 0 % |
| ducted | 3 | 0 % |
| cavitations | 3 | 0 % |
| simple | 3 | 0 % |
| 66 | 3 | 0 % |
| laboratory | 3 | 0 % |
| calculate | 3 | 0 % |
| rotor | 3 | 0 % |
| kuklinski | 3 | 0 % |
| multi | 3 | 0 % |
| n. | 2 | 0 % |
| finite | 2 | 0 % |
| serebryakov | 2 | 0 % |
| dual | 2 | 0 % |
| light | 2 | 0 % |
| karman | 2 | 0 % |
| materials | 2 | 0 % |
| energy | 2 | 0 % |
| figure | 2 | 0 % |
| threshold | 2 | 0 % |
| fraction | 2 | 0 % |
| turning | 2 | 0 % |
| ga | 2 | 0 % |
| procedure | 2 | 0 % |
| panasonic | 2 | 0 % |
| e.a.arndt | 2 | 0 % |
| prop | 2 | 0 % |
| a-konno | 2 | 0 % |
| nasa | 2 | 0 % |
| activity | 2 | 0 % |
| http | 2 | 0 % |
| future | 2 | 0 % |
| plates | 2 | 0 % |
| tech | 2 | 0 % |
| microbubble | 2 | 0 % |
| computational | 2 | 0 % |
| vertical | 2 | 0 % |
| mechanics | 2 | 0 % |
| jis | 2 | 0 % |
| stainless | 2 | 0 % |
| stutz | 2 | 0 % |
| vortices | 2 | 0 % |
| weixing | 2 | 0 % |
| transducer | 2 | 0 % |
| naca66mod | 2 | 0 % |
| numachi | 2 | 0 % |
| change | 2 | 0 % |
| density | 2 | 0 % |
| sensitivity | 2 | 0 % |
| protection | 2 | 0 % |
| front | 2 | 0 % |
| advanced | 2 | 0 % |
| influence | 2 | 0 % |
| thickness | 2 | 0 % |
| screen | 2 | 0 % |
| implosion | 2 | 0 % |
| instability | 2 | 0 % |
| www.howstuffworks.com | 2 | 0 % |
| slip | 2 | 0 % |
| 0012 | 2 | 0 % |
| fluctuations | 2 | 0 % |
| step | 2 | 0 % |
| szeri | 2 | 0 % |
| b. | 2 | 0 % |
| algorithm | 2 | 0 % |
| reducing | 2 | 0 % |
| 120 | 2 | 0 % |
| nexearch119 | 2 | 0 % |
| oscillations | 2 | 0 % |
| de | 2 | 0 % |
| flat | 2 | 0 % |
| azimuthal | 2 | 0 % |
| wing | 2 | 0 % |
| rules | 2 | 0 % |
| mehmet | 2 | 0 % |
| emission | 2 | 0 % |
| dams | 2 | 0 % |
| microjet | 2 | 0 % |
| naca0020 | 2 | 0 % |
| behavior | 2 | 0 % |
| kobe | 2 | 0 % |
| eulerian | 2 | 0 % |
| naca66 | 2 | 0 % |
| williams | 2 | 0 % |
| jtfa | 2 | 0 % |
| hull | 2 | 0 % |
| delgosha | 2 | 0 % |
| intitle | 2 | 0 % |
| panel | 2 | 0 % |
| is | 2 | 0 % |
| naval | 2 | 0 % |
| click | 2 | 0 % |
| propcav | 2 | 0 % |
| intensity | 2 | 0 % |
| breakup | 2 | 0 % |
| almost | 2 | 0 % |
| sonodynamic | 2 | 0 % |
| hydrofoils | 2 | 0 % |
| c | 2 | 0 % |
| tension | 2 | 0 % |
| rotating | 2 | 0 % |
| compressors | 2 | 0 % |
| oil | 2 | 0 % |
| fluctuation | 2 | 0 % |
| b. | 2 | 0 % |
| distance | 2 | 0 % |
| line | 2 | 0 % |
| transition | 2 | 0 % |
| francesco | 2 | 0 % |
| some | 2 | 0 % |
| motor | 2 | 0 % |
| coutier | 2 | 0 % |
| propulsion | 2 | 0 % |
| sae | 2 | 0 % |
| transfer | 2 | 0 % |
| techniques | 2 | 0 % |
| large | 2 | 0 % |
| wake | 2 | 0 % |
| greenspan-tschiegg | 2 | 0 % |
| acceleration | 2 | 0 % |
| stepped | 2 | 0 % |
| field | 2 | 0 % |
| chemical | 2 | 0 % |
| propeler | 2 | 0 % |
| fortes-patella | 2 | 0 % |
| slot | 2 | 0 % |
| stepping | 2 | 0 % |
| expansion | 2 | 0 % |
| podded | 2 | 0 % |
| boundaries | 2 | 0 % |
| salvatore | 2 | 0 % |
| pvdf | 2 | 0 % |
| lng | 2 | 0 % |
| turbulent | 2 | 0 % |
| y. | 2 | 0 % |
| acceptable | 2 | 0 % |
| waves | 2 | 0 % |
| attack | 2 | 0 % |
| cells | 2 | 0 % |
| peak | 2 | 0 % |
| resistance | 2 | 0 % |
| nnnxn | 2 | 0 % |
| interactions | 2 | 0 % |
| geometry | 2 | 0 % |
| development | 2 | 0 % |
| leipertz | 2 | 0 % |
| computations | 2 | 0 % |
| bem | 2 | 0 % |
| back | 2 | 0 % |
| h. | 2 | 0 % |
| outboard | 2 | 0 % |
| upstream | 2 | 0 % |
| 2007 | 2 | 0 % |
| scheme | 2 | 0 % |
| modified | 2 | 0 % |
| abs | 2 | 0 % |
| foam | 2 | 0 % |
| core | 2 | 0 % |
| swirl | 2 | 0 % |
| spray | 2 | 0 % |
| internal | 2 | 0 % |
| sections | 2 | 0 % |
| continuity | 2 | 0 % |
| heister | 2 | 0 % |
| work | 2 | 0 % |
| meter | 2 | 0 % |
| technologies | 2 | 0 % |
| critical | 2 | 0 % |
| roger | 2 | 0 % |
| new | 2 | 0 % |
| yamaguchi | 2 | 0 % |
| prevention | 2 | 0 % |
| three | 2 | 0 % |
| s55c | 2 | 0 % |
| transient | 2 | 0 % |
| fourth | 2 | 0 % |
| cavities | 2 | 0 % |
| 6 | 2 | 0 % |
| .edu | 2 | 0 % |
| vapour | 2 | 0 % |
| marschall | 2 | 0 % |
| eulerian/lagrangian | 2 | 0 % |
| patankar | 2 | 0 % |
| results | 2 | 0 % |
| waters | 2 | 0 % |
| – | 2 | 0 % |
| insean | 2 | 0 % |
| view | 2 | 0 % |
| formation | 2 | 0 % |
| machines | 2 | 0 % |
| therapy | 2 | 0 % |
| void | 2 | 0 % |
| shaft | 2 | 0 % |
| height | 2 | 0 % |
| navier | 2 | 0 % |
| construction | 2 | 0 % |
| synchronous | 2 | 0 % |
| mixed | 2 | 0 % |
| jules | 2 | 0 % |
| jun | 2 | 0 % |
| unstructured | 2 | 0 % |
| criteria | 2 | 0 % |
| guide | 2 | 0 % |
| full | 2 | 0 % |
| shipbuilding | 2 | 0 % |
| cav | 2 | 0 % |
| lauterborn | 2 | 0 % |
| definition | 2 | 0 % |
| takahira | 2 | 0 % |
| processing | 2 | 0 % |
| condition | 2 | 0 % |
| mark | 2 | 0 % |
| machinery | 2 | 0 % |
| phd | 2 | 0 % |
| kuiper | 2 | 0 % |
| level | 2 | 0 % |
| planktons | 2 | 0 % |
| installation | 2 | 0 % |
| root | 2 | 0 % |
| robert | 2 | 0 % |
| ashvin | 2 | 0 % |
| uncle-m | 2 | 0 % |
| evaporation | 2 | 0 % |
| near | 2 | 0 % |
| 1998 | 2 | 0 % |
| gabor | 2 | 0 % |
| r | 2 | 0 % |
| first | 2 | 0 % |
| doherty | 2 | 0 % |
| particles | 2 | 0 % |
| yakovlev | 2 | 0 % |
| sonoluminescence | 2 | 0 % |
| delivery | 1 | 0 % |
| mach | 1 | 0 % |
| form | 1 | 0 % |
| opening | 1 | 0 % |
| integrals | 1 | 0 % |
| ishida | 1 | 0 % |
| trans | 1 | 0 % |
| projectile | 1 | 0 % |
| particle | 1 | 0 % |
| 3..8 | 1 | 0 % |
| rotation | 1 | 0 % |
| ferrini | 1 | 0 % |
| leadering | 1 | 0 % |
| shapes | 1 | 0 % |
| posdunin | 1 | 0 % |
| ville | 1 | 0 % |
| inward | 1 | 0 % |
| pitting | 1 | 0 % |
| rigid | 1 | 0 % |
| lange | 1 | 0 % |
| lord | 1 | 0 % |
| g.l. | 1 | 0 % |
| counterjet | 1 | 0 % |
| stepanoff | 1 | 0 % |
| kirschner | 1 | 0 % |
| wafer | 1 | 0 % |
| sessiona5.003 | 1 | 0 % |
| equilibrium | 1 | 0 % |
| expanding | 1 | 0 % |
| practical | 1 | 0 % |
| tomita | 1 | 0 % |
| scaling | 1 | 0 % |
| system | 1 | 0 % |
| solitary | 1 | 0 % |
| cormack | 1 | 0 % |
| lips | 1 | 0 % |
| flashes | 1 | 0 % |
| incipient | 1 | 0 % |
| non-condensation | 1 | 0 % |
| dir | 1 | 0 % |
| cylinder | 1 | 0 % |
| vaporization | 1 | 0 % |
| aqua-environmental | 1 | 0 % |
| break-off | 1 | 0 % |
| maccormack | 1 | 0 % |
| bernoulli | 1 | 0 % |
| reduce | 1 | 0 % |
| various | 1 | 0 % |
| vessels | 1 | 0 % |
| a.semenov | 1 | 0 % |
| ganippa | 1 | 0 % |
| argon | 1 | 0 % |
| part | 1 | 0 % |
| photograph | 1 | 0 % |
| froude | 1 | 0 % |
| can | 1 | 0 % |
| symposiums | 1 | 0 % |
| fiber | 1 | 0 % |
| unsteady-flow | 1 | 0 % |
| predicting | 1 | 0 % |
| left | 1 | 0 % |
| helical | 1 | 0 % |
| incidence | 1 | 0 % |
| static | 1 | 0 % |
| joints | 1 | 0 % |
| cause | 1 | 0 % |
| drug | 1 | 0 % |
| guillaume | 1 | 0 % |
| leningrad | 1 | 0 % |
| viscosity | 1 | 0 % |
| re | 1 | 0 % |
| addition | 1 | 0 % |
| resonance | 1 | 0 % |
| nucleation | 1 | 0 % |
| correlation | 1 | 0 % |
| different | 1 | 0 % |
| algorithms | 1 | 0 % |
| venkateswaran | 1 | 0 % |
| project | 1 | 0 % |
| estimate | 1 | 0 % |
| lefebvre | 1 | 0 % |
| ukon | 1 | 0 % |
| problem | 1 | 0 % |
| aluminum | 1 | 0 % |
| proceedings | 1 | 0 % |
| porn | 1 | 0 % |
| mech. | 1 | 0 % |
| mohamed | 1 | 0 % |
| c. | 1 | 0 % |
| rake | 1 | 0 % |
| generators | 1 | 0 % |
| eng. | 1 | 0 % |
| karki | 1 | 0 % |
| sp-8052 | 1 | 0 % |
| 3.0 | 1 | 0 % |
| numbers | 1 | 0 % |
| rate | 1 | 0 % |
| vapor | 1 | 0 % |
| turbopumps/rocket | 1 | 0 % |
| henda | 1 | 0 % |
| distribution/ | 1 | 0 % |
| //cav2001.library.caltech.edu/ | 1 | 0 % |
| conditions | 1 | 0 % |
| source | 1 | 0 % |
| local | 1 | 0 % |
| failed | 1 | 0 % |
| spectra | 1 | 0 % |
| 0.8 | 1 | 0 % |
| dependent | 1 | 0 % |
| -venturi | 1 | 0 % |
| off-design | 1 | 0 % |
| pp | 1 | 0 % |
| 12 | 1 | 0 % |
| systematic | 1 | 0 % |
| rupture | 1 | 0 % |
| tangential | 1 | 0 % |
| artificial | 1 | 0 % |
| state | 1 | 0 % |
| pitch | 1 | 0 % |
| backscatter | 1 | 0 % |
| steam | 1 | 0 % |
| societe | 1 | 0 % |
| cav2001.library.caltech.edu/358/00/b8_006_nagahara.pdf | 1 | 0 % |
| re-entrant-jet | 1 | 0 % |
| 1973 | 1 | 0 % |
| vasin | 1 | 0 % |
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