| 820 different keywords | Search | Percent |
|---|
| cavitation | 303 | 8.8 % |
| of | 161 | 4.7 % |
| orifice | 126 | 3.6 % |
| in | 75 | 2.1 % |
| restriction | 70 | 2 % |
| and | 53 | 1.5 % |
| on | 48 | 1.4 % |
| a | 45 | 1.3 % |
| vortex | 44 | 1.2 % |
| model | 37 | 1 % |
| pdf | 37 | 1 % |
| pump | 36 | 1 % |
| the | 34 | 0.9 % |
| water | 33 | 0.9 % |
| design | 31 | 0.9 % |
| experimental | 29 | 0.8 % |
| flow | 28 | 0.8 % |
| for | 28 | 0.8 % |
| propeller | 26 | 0.7 % |
| erosion | 26 | 0.7 % |
| supercavitation | 25 | 0.7 % |
| plate | 24 | 0.7 % |
| cavitating | 22 | 0.6 % |
| study | 20 | 0.5 % |
| an | 20 | 0.5 % |
| fluent | 20 | 0.5 % |
| turbine | 19 | 0.5 % |
| tip | 19 | 0.5 % |
| effect | 19 | 0.5 % |
| hydrofoil | 17 | 0.4 % |
| cav2001 | 17 | 0.4 % |
| inducer | 17 | 0.4 % |
| numerical | 16 | 0.4 % |
| test | 16 | 0.4 % |
| filetype | 16 | 0.4 % |
| bubble | 15 | 0.4 % |
| to | 15 | 0.4 % |
| noise | 15 | 0.4 % |
| tab_hty | 14 | 0.4 % |
| cavities | 14 | 0.4 % |
| valve | 14 | 0.4 % |
| kaplan | 14 | 0.4 % |
| ventilated | 13 | 0.3 % |
| international | 13 | 0.3 % |
| cfd | 13 | 0.3 % |
| calculation | 13 | 0.3 % |
| analysis | 12 | 0.3 % |
| cavity | 12 | 0.3 % |
| dynamic | 12 | 0.3 % |
| rudder | 12 | 0.3 % |
| symposium | 11 | 0.3 % |
| pressure | 11 | 0.3 % |
| supercavitating | 11 | 0.3 % |
| simulation | 11 | 0.3 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 11 | 0.3 % |
| orifices | 11 | 0.3 % |
| method | 11 | 0.3 % |
| experiment | 10 | 0.2 % |
| number | 10 | 0.2 % |
| 2001 | 10 | 0.2 % |
| propellers | 10 | 0.2 % |
| hole | 10 | 0.2 % |
| surface | 9 | 0.2 % |
| quality | 9 | 0.2 % |
| size | 9 | 0.2 % |
| prediction | 9 | 0.2 % |
| type | 8 | 0.2 % |
| journal | 8 | 0.2 % |
| behavior | 8 | 0.2 % |
| liquid | 8 | 0.2 % |
| blade | 8 | 0.2 % |
| with | 8 | 0.2 % |
| boundary | 8 | 0.2 % |
| compressible | 8 | 0.2 % |
| engineering | 8 | 0.2 % |
| shock | 8 | 0.2 % |
| ship | 8 | 0.2 % |
| joint | 8 | 0.2 % |
| horn | 7 | 0.2 % |
| mass | 7 | 0.2 % |
| scale | 7 | 0.2 % |
| unsteady | 7 | 0.2 % |
| flows | 7 | 0.2 % |
| fluids | 7 | 0.2 % |
| template | 7 | 0.2 % |
| added | 7 | 0.2 % |
| sae | 7 | 0.2 % |
| edge | 7 | 0.2 % |
| modeling | 7 | 0.2 % |
| injection | 7 | 0.2 % |
| discharge | 7 | 0.2 % |
| wave | 7 | 0.2 % |
| characteristics | 7 | 0.2 % |
| meter | 7 | 0.2 % |
| two | 7 | 0.2 % |
| investigation | 7 | 0.2 % |
| around | 7 | 0.2 % |
| nozzle | 7 | 0.2 % |
| leading | 7 | 0.2 % |
| at | 7 | 0.2 % |
| centrifugal | 7 | 0.2 % |
| effects | 7 | 0.2 % |
| piercing | 7 | 0.2 % |
| piping | 6 | 0.1 % |
| cavitator | 6 | 0.1 % |
| hydrofoils | 6 | 0.1 % |
| rotating | 6 | 0.1 % |
| surge | 6 | 0.1 % |
| time-frequency | 6 | 0.1 % |
| or | 6 | 0.1 % |
| types | 6 | 0.1 % |
| force | 6 | 0.1 % |
| - | 6 | 0.1 % |
| clearance | 6 | 0.1 % |
| cav | 6 | 0.1 % |
| keller | 6 | 0.1 % |
| nexearch | 6 | 0.1 % |
| measurement | 5 | 0.1 % |
| scaling | 5 | 0.1 % |
| plates | 5 | 0.1 % |
| paper | 5 | 0.1 % |
| asme | 5 | 0.1 % |
| inducers | 5 | 0.1 % |
| rocket | 5 | 0.1 % |
| j. | 5 | 0.1 % |
| transactions | 5 | 0.1 % |
| maneuvering | 5 | 0.1 % |
| element | 5 | 0.1 % |
| tunnel | 5 | 0.1 % |
| modelling | 5 | 0.1 % |
| turbo | 5 | 0.1 % |
| suction | 5 | 0.1 % |
| instabilities | 5 | 0.1 % |
| installation | 5 | 0.1 % |
| submerged | 5 | 0.1 % |
| high | 5 | 0.1 % |
| azipod | 4 | 0.1 % |
| sauer | 4 | 0.1 % |
| inlet | 4 | 0.1 % |
| rate | 4 | 0.1 % |
| wing | 4 | 0.1 % |
| performance | 4 | 0.1 % |
| sound | 4 | 0.1 % |
| jet | 4 | 0.1 % |
| distribution | 4 | 0.1 % |
| introduction | 4 | 0.1 % |
| improved | 4 | 0.1 % |
| is | 4 | 0.1 % |
| coefficient | 4 | 0.1 % |
| distance | 4 | 0.1 % |
| investigations | 4 | 0.1 % |
| damage | 4 | 0.1 % |
| naca | 4 | 0.1 % |
| speed | 4 | 0.1 % |
| tank | 4 | 0.1 % |
| mechanism | 4 | 0.1 % |
| control | 4 | 0.1 % |
| three-dimensional | 4 | 0.1 % |
| gas | 4 | 0.1 % |
| sheet | 4 | 0.1 % |
| schnerr | 4 | 0.1 % |
| partial | 4 | 0.1 % |
| lattice | 4 | 0.1 % |
| kuiper | 4 | 0.1 % |
| do | 4 | 0.1 % |
| inception | 4 | 0.1 % |
| what | 3 | 0 % |
| materials | 3 | 0 % |
| turbopump | 3 | 0 % |
| marine | 3 | 0 % |
| jets | 3 | 0 % |
| by | 3 | 0 % |
| 2-d | 3 | 0 % |
| runner | 3 | 0 % |
| lithotripter | 3 | 0 % |
| dynamics | 3 | 0 % |
| heave | 3 | 0 % |
| solid | 3 | 0 % |
| drag | 3 | 0 % |
| explosion | 3 | 0 % |
| width | 3 | 0 % |
| bubbles | 3 | 0 % |
| instability | 3 | 0 % |
| focal | 3 | 0 % |
| b. | 3 | 0 % |
| similarities | 3 | 0 % |
| de | 3 | 0 % |
| elbow | 3 | 0 % |
| rules | 3 | 0 % |
| collapse | 3 | 0 % |
| stone | 3 | 0 % |
| formula | 3 | 0 % |
| dimensional | 3 | 0 % |
| cascade | 3 | 0 % |
| lecture | 3 | 0 % |
| butterfly | 3 | 0 % |
| acoustic | 3 | 0 % |
| hydrodynamic | 3 | 0 % |
| impact | 3 | 0 % |
| mtp_hty | 3 | 0 % |
| obermeier | 3 | 0 % |
| a9.006.pdf | 3 | 0 % |
| sizing | 3 | 0 % |
| angle | 3 | 0 % |
| lithotripsy | 3 | 0 % |
| treatment | 3 | 0 % |
| research | 3 | 0 % |
| npsh | 3 | 0 % |
| history | 3 | 0 % |
| orifice.pdf | 3 | 0 % |
| time | 3 | 0 % |
| comminution | 3 | 0 % |
| gust | 3 | 0 % |
| geometrical | 3 | 0 % |
| applications | 3 | 0 % |
| cryogenic | 3 | 0 % |
| using | 3 | 0 % |
| cloud | 3 | 0 % |
| methods | 3 | 0 % |
| semenenko | 3 | 0 % |
| downstream | 3 | 0 % |
| use | 3 | 0 % |
| scaled | 3 | 0 % |
| results | 3 | 0 % |
| steel | 3 | 0 % |
| conclusion | 3 | 0 % |
| p. | 3 | 0 % |
| computation | 3 | 0 % |
| rarefaction | 3 | 0 % |
| schneider | 3 | 0 % |
| session | 3 | 0 % |
| hydraulic | 3 | 0 % |
| simple | 3 | 0 % |
| vehicle | 3 | 0 % |
| frequency | 3 | 0 % |
| high-speed | 3 | 0 % |
| abstract | 3 | 0 % |
| multi | 3 | 0 % |
| closure | 2 | 0 % |
| visualizations | 2 | 0 % |
| underwater | 2 | 0 % |
| used | 2 | 0 % |
| steps | 2 | 0 % |
| energy | 2 | 0 % |
| practical | 2 | 0 % |
| phase | 2 | 0 % |
| can | 2 | 0 % |
| cores | 2 | 0 % |
| lab | 2 | 0 % |
| coefficients | 2 | 0 % |
| fluid | 2 | 0 % |
| corrosion | 2 | 0 % |
| different | 2 | 0 % |
| problem | 2 | 0 % |
| caltech | 2 | 0 % |
| stainless | 2 | 0 % |
| ductile | 2 | 0 % |
| gate | 2 | 0 % |
| perspectives | 2 | 0 % |
| change | 2 | 0 % |
| tsujimoto | 2 | 0 % |
| ratio | 2 | 0 % |
| supersonic | 2 | 0 % |
| occurs | 2 | 0 % |
| how | 2 | 0 % |
| flat | 2 | 0 % |
| vof | 2 | 0 % |
| vasin | 2 | 0 % |
| compounds | 2 | 0 % |
| technical | 2 | 0 % |
| reentrant | 2 | 0 % |
| thermal | 2 | 0 % |
| soyama | 2 | 0 % |
| sump | 2 | 0 % |
| hull | 2 | 0 % |
| oxidize | 2 | 0 % |
| hydrodynamics | 2 | 0 % |
| 1981 | 2 | 0 % |
| oscillating | 2 | 0 % |
| stokes | 2 | 0 % |
| restricted | 2 | 0 % |
| acosta | 2 | 0 % |
| 1995 | 2 | 0 % |
| ventilation | 2 | 0 % |
| free | 2 | 0 % |
| turbines | 2 | 0 % |
| foil | 2 | 0 % |
| observations | 2 | 0 % |
| layer | 2 | 0 % |
| function | 2 | 0 % |
| velocity | 2 | 0 % |
| generalized | 2 | 0 % |
| motion | 2 | 0 % |
| m/sn | 2 | 0 % |
| atlar | 2 | 0 % |
| sakoda | 2 | 0 % |
| organic | 2 | 0 % |
| location | 2 | 0 % |
| estimation | 2 | 0 % |
| theory | 2 | 0 % |
| engine | 2 | 0 % |
| turbomachinery | 2 | 0 % |
| interaction | 2 | 0 % |
| intakes | 2 | 0 % |
| reboud | 2 | 0 % |
| stones | 2 | 0 % |
| wavelet | 2 | 0 % |
| vortexing | 2 | 0 % |
| boundaries | 2 | 0 % |
| parallel | 2 | 0 % |
| aluminium | 2 | 0 % |
| turbulent | 2 | 0 % |
| waves | 2 | 0 % |
| v.n. | 2 | 0 % |
| vladimir | 2 | 0 % |
| flashing | 2 | 0 % |
| temperatures | 2 | 0 % |
| nozzles | 2 | 0 % |
| salt | 2 | 0 % |
| 0015 | 2 | 0 % |
| maximum | 2 | 0 % |
| entry | 2 | 0 % |
| apparatus | 2 | 0 % |
| drag-reduction | 2 | 0 % |
| kato | 2 | 0 % |
| d | 2 | 0 % |
| problems | 2 | 0 % |
| turbin | 2 | 0 % |
| mtb_sug.pre | 2 | 0 % |
| kidney | 2 | 0 % |
| rudders | 2 | 0 % |
| new | 2 | 0 % |
| et | 2 | 0 % |
| experiment.pdf | 2 | 0 % |
| nigmatulin | 2 | 0 % |
| pumps | 2 | 0 % |
| university | 2 | 0 % |
| target | 2 | 0 % |
| airfoil | 2 | 0 % |
| damping | 2 | 0 % |
| drawing | 2 | 0 % |
| equation | 2 | 0 % |
| conference | 2 | 0 % |
| navier | 2 | 0 % |
| curve | 2 | 0 % |
| stream | 2 | 0 % |
| adiabatic | 2 | 0 % |
| howle | 2 | 0 % |
| farhat | 2 | 0 % |
| testing | 2 | 0 % |
| micro | 2 | 0 % |
| 2d | 2 | 0 % |
| franc | 2 | 0 % |
| supercavity | 2 | 0 % |
| efficiency | 2 | 0 % |
| ships | 2 | 0 % |
| schiebe | 2 | 0 % |
| pogo | 2 | 0 % |
| from | 2 | 0 % |
| krasilnikov | 2 | 0 % |
| near | 2 | 0 % |
| 1998 | 2 | 0 % |
| hykat | 2 | 0 % |
| diameter | 2 | 0 % |
| air | 2 | 0 % |
| pumb | 1 | 0 % |
| guy | 1 | 0 % |
| n. | 1 | 0 % |
| emissions | 1 | 0 % |
| finite | 1 | 0 % |
| conventional | 1 | 0 % |
| serebryakov | 1 | 0 % |
| calculations | 1 | 0 % |
| nozzles. | 1 | 0 % |
| g.l. | 1 | 0 % |
| utilliyation | 1 | 0 % |
| equilibrium | 1 | 0 % |
| system | 1 | 0 % |
| annual | 1 | 0 % |
| incipient | 1 | 0 % |
| “partial | 1 | 0 % |
| fraction | 1 | 0 % |
| direction | 1 | 0 % |
| wind | 1 | 0 % |
| volvo | 1 | 0 % |
| investigating | 1 | 0 % |
| procedure | 1 | 0 % |
| super | 1 | 0 % |
| college | 1 | 0 % |
| 2000. | 1 | 0 % |
| g.h. | 1 | 0 % |
| helical | 1 | 0 % |
| kubota | 1 | 0 % |
| ba | 1 | 0 % |
| nasa | 1 | 0 % |
| incidence | 1 | 0 % |
| 0.3 | 1 | 0 % |
| lindau | 1 | 0 % |
| k | 1 | 0 % |
| tutorial | 1 | 0 % |
| circular-cylindrical | 1 | 0 % |
| neighbourhood | 1 | 0 % |
| navier-stokes | 1 | 0 % |
| backward-facing | 1 | 0 % |
| viscosity | 1 | 0 % |
| tx. | 1 | 0 % |
| hydrocode | 1 | 0 % |
| microhydrodynamics | 1 | 0 % |
| correlation | 1 | 0 % |
| vertical | 1 | 0 % |
| installed | 1 | 0 % |
| attached | 1 | 0 % |
| 24th | 1 | 0 % |
| resonating | 1 | 0 % |
| proceedings | 1 | 0 % |
| stutz | 1 | 0 % |
| magazine | 1 | 0 % |
| c. | 1 | 0 % |
| cavitatore | 1 | 0 % |
| there | 1 | 0 % |
| software | 1 | 0 % |
| vortices | 1 | 0 % |
| prévision | 1 | 0 % |
| 1972 | 1 | 0 % |
| “propeller | 1 | 0 % |
| pressur | 1 | 0 % |
| measured | 1 | 0 % |
| race | 1 | 0 % |
| possibility | 1 | 0 % |
| flowfields | 1 | 0 % |
| rate-dependent | 1 | 0 % |
| strong | 1 | 0 % |
| partially | 1 | 0 % |
| henda | 1 | 0 % |
| revolution | 1 | 0 % |
| lift | 1 | 0 % |
| transienten | 1 | 0 % |
| ultrasonore | 1 | 0 % |
| empirical | 1 | 0 % |
| measuring | 1 | 0 % |
| reduceing | 1 | 0 % |
| case | 1 | 0 % |
| advanced | 1 | 0 % |
| h-type | 1 | 0 % |
| multi-dimensional | 1 | 0 % |
| turbo-pump | 1 | 0 % |
| 5. | 1 | 0 % |
| institute | 1 | 0 % |
| meeting | 1 | 0 % |
| durco | 1 | 0 % |
| ellipsoid | 1 | 0 % |
| akinori | 1 | 0 % |
| laser | 1 | 0 % |
| pressures | 1 | 0 % |
| orifice? | 1 | 0 % |
| pipe | 1 | 0 % |
| nuclei | 1 | 0 % |
| step | 1 | 0 % |
| sensors | 1 | 0 % |
| down | 1 | 0 % |
| stress | 1 | 0 % |
| propulsors | 1 | 0 % |
| m3 | 1 | 0 % |
| r. | 1 | 0 % |
| propeller.pdf | 1 | 0 % |
| oscillations | 1 | 0 % |
| parameter | 1 | 0 % |
| kuzman | 1 | 0 % |
| multihole | 1 | 0 % |
| engines | 1 | 0 % |
| killing | 1 | 0 % |
| propellers. | 1 | 0 % |
| contact | 1 | 0 % |
| roosen | 1 | 0 % |
| sname | 1 | 0 % |
| multiperforated | 1 | 0 % |
| bodies | 1 | 0 % |
| 2a | 1 | 0 % |
| mehmet | 1 | 0 % |
| oforifices | 1 | 0 % |
| pumping | 1 | 0 % |
| crash-stop | 1 | 0 % |
| emission | 1 | 0 % |
| radius | 1 | 0 % |
| oscillation | 1 | 0 % |
| freesurface | 1 | 0 % |
| / | 1 | 0 % |
| which | 1 | 0 % |
| & | 1 | 0 % |
| cavitational | 1 | 0 % |
| cpecs | 1 | 0 % |
| y | 1 | 0 % |
| river | 1 | 0 % |
| grenoble | 1 | 0 % |
| regiane | 1 | 0 % |
| injectors | 1 | 0 % |
| cone | 1 | 0 % |
| kerwin | 1 | 0 % |
| d.zhang | 1 | 0 % |
| fences | 1 | 0 % |
| weakly | 1 | 0 % |
| ps | 1 | 0 % |
| download | 1 | 0 % |
| savchenko | 1 | 0 % |
| over | 1 | 0 % |
| visualization | 1 | 0 % |
| panel | 1 | 0 % |
| patella | 1 | 0 % |
| photographer | 1 | 0 % |
| diffuser | 1 | 0 % |
| properetti | 1 | 0 % |
| station | 1 | 0 % |
| prevent | 1 | 0 % |
| willis | 1 | 0 % |
| astm | 1 | 0 % |
| index | 1 | 0 % |
| length | 1 | 0 % |
| 0.5 | 1 | 0 % |
| deynekin | 1 | 0 % |
| two-phase | 1 | 0 % |
| j.m. | 1 | 0 % |
| valves | 1 | 0 % |
| gindroz | 1 | 0 % |
| “ten | 1 | 0 % |
| ” | 1 | 0 % |
| propellor | 1 | 0 % |
| bulle | 1 | 0 % |
| unstable | 1 | 0 % |
| formulation | 1 | 0 % |
| induser | 1 | 0 % |
| upsteam | 1 | 0 % |
| eddy | 1 | 0 % |
| wedge | 1 | 0 % |
| papers | 1 | 0 % |
| champ | 1 | 0 % |
| sketch | 1 | 0 % |
| 1982 | 1 | 0 % |
| trubulent | 1 | 0 % |
| surface-piercing | 1 | 0 % |
| undersuchung | 1 | 0 % |
| anti | 1 | 0 % |
| singhal | 1 | 0 % |
| m | 1 | 0 % |
| through | 1 | 0 % |
| oil | 1 | 0 % |
| hattori | 1 | 0 % |
| theoretical | 1 | 0 % |
| djeridi | 1 | 0 % |
| effectives | 1 | 0 % |
| table | 1 | 0 % |
| brix | 1 | 0 % |
| cavitaiton | 1 | 0 % |
| utilization | 1 | 0 % |
| transition | 1 | 0 % |
| determined | 1 | 0 % |
| quality#sclient=psy | 1 | 0 % |
| 1.5 | 1 | 0 % |
| secondary | 1 | 0 % |
| applied | 1 | 0 % |
| some | 1 | 0 % |
| pulse | 1 | 0 % |
| measurements | 1 | 0 % |
| ballast | 1 | 0 % |
| catalog | 1 | 0 % |
| bearing | 1 | 0 % |
| a8 | 1 | 0 % |
| advantages | 1 | 0 % |
| a&m | 1 | 0 % |
| libraries | 1 | 0 % |
| coutier | 1 | 0 % |
| yu | 1 | 0 % |
| transfer | 1 | 0 % |
| boss | 1 | 0 % |
| large | 1 | 0 % |
| berntsen | 1 | 0 % |
| modelierung | 1 | 0 % |
| e.-a. | 1 | 0 % |
| berchiche | 1 | 0 % |
| hands | 1 | 0 % |
| gravitational | 1 | 0 % |
| missile | 1 | 0 % |
| field | 1 | 0 % |
| brennen | 1 | 0 % |
| karlan | 1 | 0 % |
| representation | 1 | 0 % |
| matlab | 1 | 0 % |
| fortes | 1 | 0 % |
| utilization | 1 | 0 % |
| s. | 1 | 0 % |
| kinnas | 1 | 0 % |
| hr | 1 | 0 % |
| okamura | 1 | 0 % |
| elrod | 1 | 0 % |
| furukawa | 1 | 0 % |
| degree | 1 | 0 % |
| midchord | 1 | 0 % |
| fortes-patella | 1 | 0 % |
| . | 1 | 0 % |
| tullis | 1 | 0 % |
| l.g. | 1 | 0 % |
| long | 1 | 0 % |
| example | 1 | 0 % |
| between | 1 | 0 % |
| working | 1 | 0 % |
| sbsl | 1 | 0 % |
| application | 1 | 0 % |
| without | 1 | 0 % |
| laws | 1 | 0 % |
| space | 1 | 0 % |
| constants | 1 | 0 % |
| l | 1 | 0 % |
| videos | 1 | 0 % |
| podded | 1 | 0 % |
| orifice= | 1 | 0 % |
| mm | 1 | 0 % |
| taper | 1 | 0 % |
| applicable | 1 | 0 % |
| guzevsky | 1 | 0 % |
| kyushu | 1 | 0 % |
| re-entrant | 1 | 0 % |
| y. | 1 | 0 % |
| reduction | 1 | 0 % |
| technology | 1 | 0 % |
| attack | 1 | 0 % |
| steady | 1 | 0 % |
| rings | 1 | 0 % |
| sigma | 1 | 0 % |
| 2000 | 1 | 0 % |
| dispersion | 1 | 0 % |
| levels | 1 | 0 % |
| calc | 1 | 0 % |
| secret | 1 | 0 % |
| mpuf | 1 | 0 % |
| resistance | 1 | 0 % |
| design-analysis | 1 | 0 % |
| stability | 1 | 0 % |
| azipods | 1 | 0 % |
| relief | 1 | 0 % |
| bellmouth | 1 | 0 % |
| friesch | 1 | 0 % |
| france | 1 | 0 % |
| cfdrc | 1 | 0 % |
| hyderphoile#q=dynamic | 1 | 0 % |
| saturated | 1 | 0 % |
| geometry | 1 | 0 % |
| diagram | 1 | 0 % |
| piv | 1 | 0 % |
| data | 1 | 0 % |
| jowkovski | 1 | 0 % |
| senocak | 1 | 0 % |
| des | 1 | 0 % |
| vibration | 1 | 0 % |
| supercavitation–problems | 1 | 0 % |
| ecoulement | 1 | 0 % |
| after | 1 | 0 % |
| Гузевский | 1 | 0 % |
| manoeuvring | 1 | 0 % |
| computations | 1 | 0 % |
| cd | 1 | 0 % |
| rebounce | 1 | 0 % |
| mitigate | 1 | 0 % |
| tait | 1 | 0 % |
| breaks | 1 | 0 % |
| as | 1 | 0 % |
| quantitative | 1 | 0 % |
| bacteria | 1 | 0 % |
| cavitation-bubble | 1 | 0 % |
| 5 | 1 | 0 % |
| india | 1 | 0 % |
| manual | 1 | 0 % |
| third | 1 | 0 % |
| shear | 1 | 0 % |
| upstream | 1 | 0 % |
| 65-006 | 1 | 0 % |
| theory-propeller.pdf | 1 | 0 % |
| reason | 1 | 0 % |
| throttled | 1 | 0 % |
| savineau | 1 | 0 % |
| al | 1 | 0 % |
| abs | 1 | 0 % |
| modified | 1 | 0 % |
| 1997 | 1 | 0 % |
| penta | 1 | 0 % |
| anton | 1 | 0 % |
| span | 1 | 0 % |
| fortran | 1 | 0 % |
| magnetic | 1 | 0 % |
| specific | 1 | 0 % |
| review” | 1 | 0 % |
| allowable | 1 | 0 % |
| body | 1 | 0 % |
| colloquium | 1 | 0 % |
| spray | 1 | 0 % |
| for? | 1 | 0 % |
| bottom | 1 | 0 % |
| turbomachines | 1 | 0 % |
| setup | 1 | 0 % |
| qaulity | 1 | 0 % |
| american | 1 | 0 % |
| multiple | 1 | 0 % |
| approach | 1 | 0 % |
| orofice | 1 | 0 % |
| negetive | 1 | 0 % |
| ariane | 1 | 0 % |
| chahine | 1 | 0 % |
| critical | 1 | 0 % |
| singularity | 1 | 0 % |
| streams | 1 | 0 % |
| perliminary | 1 | 0 % |
| evaluation | 1 | 0 % |
| hydrostatic | 1 | 0 % |
| professor | 1 | 0 % |
| mouthpiece | 1 | 0 % |
| stations | 1 | 0 % |
| chimera | 1 | 0 % |
| “fluid | 1 | 0 % |
| o. | 1 | 0 % |
| engineering#sclient=psy | 1 | 0 % |
| term | 1 | 0 % |
| lakshminarayana | 1 | 0 % |
| simulations | 1 | 0 % |
| venturi | 1 | 0 % |
| fourth | 1 | 0 % |
| couplage | 1 | 0 % |
| stoffel | 1 | 0 % |
| vapour | 1 | 0 % |
| turbulence | 1 | 0 % |
| delale | 1 | 0 % |
| rictiction | 1 | 0 % |
| diverging | 1 | 0 % |
| diesel | 1 | 0 % |
| vol. | 1 | 0 % |
| hard-over | 1 | 0 % |
| hitoshi | 1 | 0 % |
| matériau | 1 | 0 % |
| 00 | 1 | 0 % |
| area | 1 | 0 % |
| void | 1 | 0 % |
| forces | 1 | 0 % |
| w. | 1 | 0 % |
| indices | 1 | 0 % |
| weitendorf | 1 | 0 % |
| shaft | 1 | 0 % |
| godfred | 1 | 0 % |
| transform | 1 | 0 % |
| integral | 1 | 0 % |
| shuji | 1 | 0 % |
| species | 1 | 0 % |
| krylov | 1 | 0 % |
| japan | 1 | 0 % |
| profile | 1 | 0 % |
| jules | 1 | 0 % |
| predict | 1 | 0 % |
| yuan | 1 | 0 % |
| detachment | 1 | 0 % |
| generated | 1 | 0 % |
| govindarajan | 1 | 0 % |
| vane | 1 | 0 % |
| head | 1 | 0 % |
| star | 1 | 0 % |
| guide | 1 | 0 % |
| cav2006 | 1 | 0 % |
| modélisation | 1 | 0 % |
| fission | 1 | 0 % |
| inanc | 1 | 0 % |
| shipbuilding | 1 | 0 % |
| ultrasonic | 1 | 0 % |
| 104/411 | 1 | 0 % |
| j.p. | 1 | 0 % |
| fifth | 1 | 0 % |
| coeff.v/nd | 1 | 0 % |
| hirschi | 1 | 0 % |
| 1956 | 1 | 0 % |
| texas | 1 | 0 % |
| nitrogen | 1 | 0 % |
| 1st | 1 | 0 % |
| fmfuru@mech.kyushu-u.ac.jp | 1 | 0 % |
| -300 | 1 | 0 % |
| luminescence | 1 | 0 % |
| plesset | 1 | 0 % |
| years | 1 | 0 % |
| machinery | 1 | 0 % |
| nozzel | 1 | 0 % |
| compared | 1 | 0 % |
| configuration | 1 | 0 % |
| characteristic | 1 | 0 % |
| spectrum | 1 | 0 % |
| cavitations | 1 | 0 % |
| kawanami | 1 | 0 % |
| retriction | 1 | 0 % |
| single-blade | 1 | 0 % |
| mitchell | 1 | 0 % |
| sources | 1 | 0 % |
| dissipators | 1 | 0 % |
| resistant | 1 | 0 % |
| differentiation | 1 | 0 % |
| drop | 1 | 0 % |
| kyowa-pgm-2kc | 1 | 0 % |
| homogeneous | 1 | 0 % |
| 1978 | 1 | 0 % |
| michel | 1 | 0 % |
| 3rd | 1 | 0 % |
| paris | 1 | 0 % |
| hemisperical | 1 | 0 % |
| eliminating | 1 | 0 % |
| tunnels.pdf | 1 | 0 % |
| be | 1 | 0 % |
| dumont | 1 | 0 % |
| instruction | 1 | 0 % |
| dipole | 1 | 0 % |
| chandrashekhara | 1 | 0 % |
| mail | 1 | 0 % |
| towing | 1 | 0 % |
| 3 | 1 | 0 % |
| analyze | 1 | 0 % |
| al. | 1 | 0 % |
| structure | 1 | 0 % |
| isa | 1 | 0 % |
| exponent | 1 | 0 % |
| Other words | 2 | 0 % |
|