| 1328 different keywords | Search | Percent |
|---|
| cavitation | 520 | 9.5 % |
| of | 156 | 2.8 % |
| pdf | 128 | 2.3 % |
| propeller | 124 | 2.2 % |
| pump | 94 | 1.7 % |
| orifice | 59 | 1 % |
| flow | 56 | 1 % |
| in | 52 | 0.9 % |
| centrifugal | 52 | 0.9 % |
| fluent | 46 | 0.8 % |
| bubble | 45 | 0.8 % |
| on | 44 | 0.8 % |
| and | 41 | 0.7 % |
| vortex | 41 | 0.7 % |
| filetype | 39 | 0.7 % |
| supercavitation | 38 | 0.6 % |
| model | 36 | 0.6 % |
| erosion | 35 | 0.6 % |
| a | 34 | 0.6 % |
| restriction | 34 | 0.6 % |
| the | 34 | 0.6 % |
| water | 32 | 0.5 % |
| pressure | 30 | 0.5 % |
| supercavitating | 29 | 0.5 % |
| numerical | 28 | 0.5 % |
| number | 27 | 0.4 % |
| analysis | 27 | 0.4 % |
| ship | 27 | 0.4 % |
| equation | 26 | 0.4 % |
| propellers | 25 | 0.4 % |
| suction | 23 | 0.4 % |
| jet | 22 | 0.4 % |
| cavitating | 22 | 0.4 % |
| surface | 21 | 0.3 % |
| simulation | 21 | 0.3 % |
| blade | 20 | 0.3 % |
| noise | 20 | 0.3 % |
| bubbles | 19 | 0.3 % |
| inducer | 19 | 0.3 % |
| for | 19 | 0.3 % |
| turbine | 18 | 0.3 % |
| experimental | 18 | 0.3 % |
| tip | 17 | 0.3 % |
| design | 17 | 0.3 % |
| valve | 17 | 0.3 % |
| method | 17 | 0.3 % |
| kaplan | 17 | 0.3 % |
| phase | 16 | 0.2 % |
| video | 16 | 0.2 % |
| to | 16 | 0.2 % |
| boundary | 16 | 0.2 % |
| modeling | 16 | 0.2 % |
| tunnel | 16 | 0.2 % |
| hydraulic | 16 | 0.2 % |
| rudder | 16 | 0.2 % |
| effects | 16 | 0.2 % |
| laser | 15 | 0.2 % |
| hydrodynamic | 15 | 0.2 % |
| hydrofoil | 15 | 0.2 % |
| velocity | 15 | 0.2 % |
| wave | 15 | 0.2 % |
| pumps | 15 | 0.2 % |
| nozzle | 15 | 0.2 % |
| frequency | 15 | 0.2 % |
| calculation | 15 | 0.2 % |
| energy | 13 | 0.2 % |
| test | 13 | 0.2 % |
| sheet | 13 | 0.2 % |
| cfd | 13 | 0.2 % |
| effect | 13 | 0.2 % |
| piercing | 13 | 0.2 % |
| azipod | 12 | 0.2 % |
| fluid | 12 | 0.2 % |
| symposium | 12 | 0.2 % |
| coefficient | 12 | 0.2 % |
| with | 12 | 0.2 % |
| rocket | 12 | 0.2 % |
| or | 12 | 0.2 % |
| impeller | 12 | 0.2 % |
| vibration | 12 | 0.2 % |
| turbopump | 11 | 0.2 % |
| super | 11 | 0.2 % |
| drag | 11 | 0.2 % |
| unsteady | 11 | 0.2 % |
| cavitator | 11 | 0.2 % |
| theory | 11 | 0.2 % |
| naca | 11 | 0.2 % |
| time | 11 | 0.2 % |
| thesis | 11 | 0.2 % |
| cavity | 11 | 0.2 % |
| size | 11 | 0.2 % |
| rayleigh | 11 | 0.2 % |
| author | 10 | 0.1 % |
| dynamics | 10 | 0.1 % |
| how | 10 | 0.1 % |
| control | 10 | 0.1 % |
| international | 10 | 0.1 % |
| diesel | 10 | 0.1 % |
| 2d | 10 | 0.1 % |
| diameter | 10 | 0.1 % |
| type | 9 | 0.1 % |
| pipe | 9 | 0.1 % |
| is | 9 | 0.1 % |
| flows | 9 | 0.1 % |
| butterfly | 9 | 0.1 % |
| stokes | 9 | 0.1 % |
| cav2001 | 9 | 0.1 % |
| 3d | 9 | 0.1 % |
| speed | 9 | 0.1 % |
| .pdf | 9 | 0.1 % |
| mass | 8 | 0.1 % |
| rayleigh-plesset | 8 | 0.1 % |
| wake | 8 | 0.1 % |
| vladimir | 8 | 0.1 % |
| plate | 8 | 0.1 % |
| turbulence | 8 | 0.1 % |
| joint | 8 | 0.1 % |
| krasilnikov | 8 | 0.1 % |
| air | 8 | 0.1 % |
| horn | 7 | 0.1 % |
| marine | 7 | 0.1 % |
| study | 7 | 0.1 % |
| models | 7 | 0.1 % |
| bell | 7 | 0.1 % |
| liquid | 7 | 0.1 % |
| cone | 7 | 0.1 % |
| foil | 7 | 0.1 % |
| types | 7 | 0.1 % |
| turbin | 7 | 0.1 % |
| two | 7 | 0.1 % |
| induced | 7 | 0.1 % |
| cav | 7 | 0.1 % |
| around | 7 | 0.1 % |
| plesset | 7 | 0.1 % |
| lattice | 7 | 0.1 % |
| ships | 7 | 0.1 % |
| near | 7 | 0.1 % |
| at | 7 | 0.1 % |
| studies | 7 | 0.1 % |
| picture | 7 | 0.1 % |
| materials | 6 | 0.1 % |
| curves | 6 | 0.1 % |
| computational | 6 | 0.1 % |
| ductile | 6 | 0.1 % |
| density | 6 | 0.1 % |
| 120 | 6 | 0.1 % |
| distribution | 6 | 0.1 % |
| hydrofoils | 6 | 0.1 % |
| aisi | 6 | 0.1 % |
| pictures | 6 | 0.1 % |
| injection | 6 | 0.1 % |
| development | 6 | 0.1 % |
| as | 6 | 0.1 % |
| shock | 6 | 0.1 % |
| characteristics | 6 | 0.1 % |
| japikse | 6 | 0.1 % |
| steel | 6 | 0.1 % |
| viscous | 6 | 0.1 % |
| airfoil | 6 | 0.1 % |
| integral | 6 | 0.1 % |
| orifices | 6 | 0.1 % |
| drop | 6 | 0.1 % |
| inception | 6 | 0.1 % |
| nexearch | 6 | 0.1 % |
| what | 5 | 0 % |
| calculations | 5 | 0 % |
| underwater | 5 | 0 % |
| by | 5 | 0 % |
| proceedings | 5 | 0 % |
| means | 5 | 0 % |
| inlet | 5 | 0 % |
| equations | 5 | 0 % |
| solid | 5 | 0 % |
| injector | 5 | 0 % |
| journal | 5 | 0 % |
| intake | 5 | 0 % |
| reducing | 5 | 0 % |
| vof | 5 | 0 % |
| collapse | 5 | 0 % |
| soyama | 5 | 0 % |
| 2001 | 5 | 0 % |
| savchenko | 5 | 0 % |
| propellor | 5 | 0 % |
| free | 5 | 0 % |
| inducers | 5 | 0 % |
| ventilated | 5 | 0 % |
| bearing | 5 | 0 % |
| angle | 5 | 0 % |
| david | 5 | 0 % |
| damage | 5 | 0 % |
| npsh | 5 | 0 % |
| les | 5 | 0 % |
| multiphase | 5 | 0 % |
| section | 5 | 0 % |
| use | 5 | 0 % |
| cavities | 5 | 0 % |
| volume | 5 | 0 % |
| prediction | 5 | 0 % |
| generator | 5 | 0 % |
| logvinovich | 5 | 0 % |
| modelling | 5 | 0 % |
| head | 5 | 0 % |
| growth | 5 | 0 % |
| potential | 5 | 0 % |
| keller | 5 | 0 % |
| site | 5 | 0 % |
| kuklinski | 5 | 0 % |
| high | 5 | 0 % |
| scaling | 4 | 0 % |
| bernoulli | 4 | 0 % |
| ganippa | 4 | 0 % |
| prop | 4 | 0 % |
| helical | 4 | 0 % |
| plates | 4 | 0 % |
| viscosity | 4 | 0 % |
| 1015 | 4 | 0 % |
| vortices | 4 | 0 % |
| kyowa | 4 | 0 % |
| change | 4 | 0 % |
| implicit | 4 | 0 % |
| partially | 4 | 0 % |
| ca | 4 | 0 % |
| thickness | 4 | 0 % |
| ittc | 4 | 0 % |
| roll | 4 | 0 % |
| state | 4 | 0 % |
| skew | 4 | 0 % |
| scale | 4 | 0 % |
| up | 4 | 0 % |
| multiperforated | 4 | 0 % |
| behavior | 4 | 0 % |
| oscillation | 4 | 0 % |
| performance | 4 | 0 % |
| formed | 4 | 0 % |
| georges | 4 | 0 % |
| & | 4 | 0 % |
| ultrasonics | 4 | 0 % |
| injectors | 4 | 0 % |
| vibrations | 4 | 0 % |
| introduction | 4 | 0 % |
| intitle | 4 | 0 % |
| panel | 4 | 0 % |
| pasadena | 4 | 0 % |
| index | 4 | 0 % |
| oscillating | 4 | 0 % |
| two-phase | 4 | 0 % |
| turbines | 4 | 0 % |
| propulsion | 4 | 0 % |
| vessel | 4 | 0 % |
| hydro | 4 | 0 % |
| an | 4 | 0 % |
| merkle | 4 | 0 % |
| atlar | 4 | 0 % |
| dissipation | 4 | 0 % |
| engine | 4 | 0 % |
| turbomachinery | 4 | 0 % |
| degree | 4 | 0 % |
| compressible | 4 | 0 % |
| are | 4 | 0 % |
| application | 4 | 0 % |
| force | 4 | 0 % |
| boundaries | 4 | 0 % |
| strouhal | 4 | 0 % |
| steady | 4 | 0 % |
| nozzles | 4 | 0 % |
| geometry | 4 | 0 % |
| mechanism | 4 | 0 % |
| problems | 4 | 0 % |
| swirl | 4 | 0 % |
| spray | 4 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 4 | 0 % |
| rudders | 4 | 0 % |
| chahine | 4 | 0 % |
| critical | 4 | 0 % |
| evaluation | 4 | 0 % |
| transient | 4 | 0 % |
| francis | 4 | 0 % |
| dynamic | 4 | 0 % |
| properties | 4 | 0 % |
| thrust | 4 | 0 % |
| s | 4 | 0 % |
| rig | 4 | 0 % |
| spectrum | 4 | 0 % |
| usa | 4 | 0 % |
| photos | 4 | 0 % |
| 3 | 4 | 0 % |
| finite | 3 | 0 % |
| particle | 3 | 0 % |
| figure | 3 | 0 % |
| thermodynamic | 3 | 0 % |
| penetration | 3 | 0 % |
| navier-stokes | 3 | 0 % |
| re | 3 | 0 % |
| camber | 3 | 0 % |
| weixing | 3 | 0 % |
| laminar | 3 | 0 % |
| numbers | 3 | 0 % |
| taib | 3 | 0 % |
| vapor | 3 | 0 % |
| supersonic | 3 | 0 % |
| performance\ | 3 | 0 % |
| artificial | 3 | 0 % |
| oscillations | 3 | 0 % |
| parameter | 3 | 0 % |
| entrant | 3 | 0 % |
| flat | 3 | 0 % |
| pumping | 3 | 0 % |
| microjet | 3 | 0 % |
| technical | 3 | 0 % |
| thermal | 3 | 0 % |
| formula | 3 | 0 % |
| g.v. | 3 | 0 % |
| sump | 3 | 0 % |
| patella | 3 | 0 % |
| fluids | 3 | 0 % |
| paper | 3 | 0 % |
| sous | 3 | 0 % |
| cascade | 3 | 0 % |
| astm | 3 | 0 % |
| pellone | 3 | 0 % |
| 2001. | 3 | 0 % |
| parameters | 3 | 0 % |
| rotating | 3 | 0 % |
| formulation | 3 | 0 % |
| immersion | 3 | 0 % |
| loading | 3 | 0 % |
| similarity | 3 | 0 % |
| layer | 3 | 0 % |
| added | 3 | 0 % |
| coutier | 3 | 0 % |
| time-frequency | 3 | 0 % |
| large | 3 | 0 % |
| arndt | 3 | 0 % |
| rebattet | 3 | 0 % |
| shape | 3 | 0 % |
| interaction | 3 | 0 % |
| intakes | 3 | 0 % |
| june | 3 | 0 % |
| code | 3 | 0 % |
| history | 3 | 0 % |
| turbulent | 3 | 0 % |
| j. | 3 | 0 % |
| waves | 3 | 0 % |
| reduction | 3 | 0 % |
| cylindrical | 3 | 0 % |
| - | 3 | 0 % |
| zero | 3 | 0 % |
| tank | 3 | 0 % |
| 0015 | 3 | 0 % |
| senocak | 3 | 0 % |
| maximum | 3 | 0 % |
| manoeuvring | 3 | 0 % |
| tait | 3 | 0 % |
| 5 | 3 | 0 % |
| manual | 3 | 0 % |
| supercavitaion | 3 | 0 % |
| hosangadi | 3 | 0 % |
| body | 3 | 0 % |
| ariane | 3 | 0 % |
| methods | 3 | 0 % |
| strategies | 3 | 0 % |
| throat | 3 | 0 % |
| venturi | 3 | 0 % |
| fourth | 3 | 0 % |
| stoffel | 3 | 0 % |
| hanseong | 3 | 0 % |
| enhance | 3 | 0 % |
| burrill | 3 | 0 % |
| lubrication | 3 | 0 % |
| christian | 3 | 0 % |
| discharging | 3 | 0 % |
| clearance | 3 | 0 % |
| conference | 3 | 0 % |
| navier | 3 | 0 % |
| tplox | 3 | 0 % |
| yuan | 3 | 0 % |
| p. | 3 | 0 % |
| balistique | 3 | 0 % |
| parsons | 3 | 0 % |
| tulin | 3 | 0 % |
| cpp | 3 | 0 % |
| condition | 3 | 0 % |
| hydrophone | 3 | 0 % |
| ball | 3 | 0 % |
| loss | 3 | 0 % |
| characteristic | 3 | 0 % |
| kawanami | 3 | 0 % |
| edu | 3 | 0 % |
| robert | 3 | 0 % |
| material | 3 | 0 % |
| cross | 3 | 0 % |
| 1055 | 3 | 0 % |
| high-speed | 3 | 0 % |
| hammer | 3 | 0 % |
| report | 3 | 0 % |
| submerged | 3 | 0 % |
| rotation | 2 | 0 % |
| karman | 2 | 0 % |
| gravity | 2 | 0 % |
| contraction | 2 | 0 % |
| system | 2 | 0 % |
| wall | 2 | 0 % |
| lips | 2 | 0 % |
| cylinder | 2 | 0 % |
| yuriy | 2 | 0 % |
| g32 | 2 | 0 % |
| jets | 2 | 0 % |
| crests | 2 | 0 % |
| carolyn | 2 | 0 % |
| t. | 2 | 0 % |
| star-cd | 2 | 0 % |
| experiment | 2 | 0 % |
| static | 2 | 0 % |
| crest | 2 | 0 % |
| j-blake | 2 | 0 % |
| 1974 | 2 | 0 % |
| aluminum | 2 | 0 % |
| mechanics | 2 | 0 % |
| grid | 2 | 0 % |
| tamura | 2 | 0 % |
| rake | 2 | 0 % |
| heat | 2 | 0 % |
| slipstream | 2 | 0 % |
| analyses | 2 | 0 % |
| weber | 2 | 0 % |
| g.kuiper | 2 | 0 % |
| fundamental | 2 | 0 % |
| kavitation | 2 | 0 % |
| lift | 2 | 0 % |
| conditions | 2 | 0 % |
| series | 2 | 0 % |
| mouth | 2 | 0 % |
| ratio | 2 | 0 % |
| judge | 2 | 0 % |
| institute | 2 | 0 % |
| causes | 2 | 0 % |
| yoshiaki | 2 | 0 % |
| minnesota | 2 | 0 % |
| www.howstuffworks.com | 2 | 0 % |
| about | 2 | 0 % |
| algorithm | 2 | 0 % |
| similarities | 2 | 0 % |
| ring | 2 | 0 % |
| tunnels | 2 | 0 % |
| de | 2 | 0 % |
| killing | 2 | 0 % |
| pgm | 2 | 0 % |
| 2kc | 2 | 0 % |
| wing | 2 | 0 % |
| vasin | 2 | 0 % |
| radius | 2 | 0 % |
| capacity | 2 | 0 % |
| photo | 2 | 0 % |
| degrees | 2 | 0 % |
| rpm | 2 | 0 % |
| fine | 2 | 0 % |
| rayleigh–plesset | 2 | 0 % |
| sound | 2 | 0 % |
| hull | 2 | 0 % |
| mccormick | 2 | 0 % |
| oscillatory | 2 | 0 % |
| over | 2 | 0 % |
| visualization | 2 | 0 % |
| english | 2 | 0 % |
| cfl | 2 | 0 % |
| pipes | 2 | 0 % |
| hydrodynamics | 2 | 0 % |
| sonic | 2 | 0 % |
| [pdf] | 2 | 0 % |
| plankton | 2 | 0 % |
| g. | 2 | 0 % |
| stanyukovich | 2 | 0 % |
| cav2001.library.caltech.edu/80/01/yuan_schnerr.ps | 2 | 0 % |
| wavelength | 2 | 0 % |
| webkr | 2 | 0 % |
| lovik | 2 | 0 % |
| ventilation | 2 | 0 % |
| impact | 2 | 0 % |
| xiaolangdi | 2 | 0 % |
| planing | 2 | 0 % |
| asme | 2 | 0 % |
| jessup | 2 | 0 % |
| m | 2 | 0 % |
| industry | 2 | 0 % |
| theoretical | 2 | 0 % |
| prandtl-meyer | 2 | 0 % |
| bernd | 2 | 0 % |
| layout | 2 | 0 % |
| line | 2 | 0 % |
| observations | 2 | 0 % |
| function | 2 | 0 % |
| linear | 2 | 0 % |
| residual | 2 | 0 % |
| face | 2 | 0 % |
| transfer | 2 | 0 % |
| cooper | 2 | 0 % |
| diffusor | 2 | 0 % |
| inflow | 2 | 0 % |
| wings | 2 | 0 % |
| brennen | 2 | 0 % |
| fortes | 2 | 0 % |
| reynolds | 2 | 0 % |
| pod | 2 | 0 % |
| solver | 2 | 0 % |
| sumino | 2 | 0 % |
| analysys | 2 | 0 % |
| young | 2 | 0 % |
| . | 2 | 0 % |
| physical | 2 | 0 % |
| breakdown | 2 | 0 % |
| reboud | 2 | 0 % |
| stagnation | 2 | 0 % |
| videos | 2 | 0 % |
| saturation | 2 | 0 % |
| clark-y | 2 | 0 % |
| olofsson | 2 | 0 % |
| period | 2 | 0 % |
| consideration | 2 | 0 % |
| technology | 2 | 0 % |
| ohl | 2 | 0 % |
| strength | 2 | 0 % |
| sigma | 2 | 0 % |
| variation | 2 | 0 % |
| pass | 2 | 0 % |
| draw | 2 | 0 % |
| rebound | 2 | 0 % |
| rea | 2 | 0 % |
| image | 2 | 0 % |
| formed? | 2 | 0 % |
| vibration. | 2 | 0 % |
| mixture | 2 | 0 % |
| combustion | 2 | 0 % |
| impellers | 2 | 0 % |
| spherical | 2 | 0 % |
| factor | 2 | 0 % |
| baiter | 2 | 0 % |
| cp | 2 | 0 % |
| pattern | 2 | 0 % |
| quantitative | 2 | 0 % |
| spillway | 2 | 0 % |
| boats | 2 | 0 % |
| 2. | 2 | 0 % |
| shear | 2 | 0 % |
| ultrasound | 2 | 0 % |
| d | 2 | 0 % |
| 2007 | 2 | 0 % |
| maneuvering | 2 | 0 % |
| engineering | 2 | 0 % |
| designer | 2 | 0 % |
| element | 2 | 0 % |
| 1997 | 2 | 0 % |
| m. | 2 | 0 % |
| single | 2 | 0 % |
| permeability | 2 | 0 % |
| chen | 2 | 0 % |
| cloud | 2 | 0 % |
| smoothing | 2 | 0 % |
| cvg | 2 | 0 % |
| matsumoto | 2 | 0 % |
| duration | 2 | 0 % |
| semenenko | 2 | 0 % |
| blake | 2 | 0 % |
| pfleiderer | 2 | 0 % |
| s55c | 2 | 0 % |
| stuart | 2 | 0 % |
| university | 2 | 0 % |
| n | 2 | 0 % |
| derivation | 2 | 0 % |
| 11.7% | 2 | 0 % |
| celerity | 2 | 0 % |
| gas | 2 | 0 % |
| nicolas | 2 | 0 % |
| forces | 2 | 0 % |
| k. | 2 | 0 % |
| weitendorf | 2 | 0 % |
| thruster | 2 | 0 % |
| throttling | 2 | 0 % |
| jean-pierre | 2 | 0 % |
| correction | 2 | 0 % |
| turbo | 2 | 0 % |
| crash | 2 | 0 % |
| profile | 2 | 0 % |
| 2 | 2 | 0 % |
| marin | 2 | 0 % |
| criteria | 2 | 0 % |
| gowing | 2 | 0 % |
| partial | 2 | 0 % |
| toyo | 2 | 0 % |
| 2. simulation | 2 | 0 % |
| instabilities | 2 | 0 % |
| i | 2 | 0 % |
| mean | 2 | 0 % |
| labview | 2 | 0 % |
| nitrogen | 2 | 0 % |
| sonochemistry | 2 | 0 % |
| kinematic | 2 | 0 % |
| micro | 2 | 0 % |
| who | 2 | 0 % |
| franc | 2 | 0 % |
| q | 2 | 0 % |
| vs. | 2 | 0 % |
| range | 2 | 0 % |
| alternate | 2 | 0 % |
| homogeneous | 2 | 0 % |
| 1978 | 2 | 0 % |
| ashvin | 2 | 0 % |
| preconditioned | 2 | 0 % |
| mid-chord | 2 | 0 % |
| song | 2 | 0 % |
| 1917 | 2 | 0 % |
| dumont | 2 | 0 % |
| vorticity | 2 | 0 % |
| noises | 2 | 0 % |
| barotropic | 2 | 0 % |
| l. | 2 | 0 % |
| foils | 2 | 0 % |
| analyze | 2 | 0 % |
| particles | 2 | 0 % |
| structure | 2 | 0 % |
| multi | 2 | 0 % |
| rolla | 2 | 0 % |
| sonoluminescence | 2 | 0 % |
| mpa | 1 | 0 % |
| mach | 1 | 0 % |
| form | 1 | 0 % |
| philos | 1 | 0 % |
| circuits | 1 | 0 % |
| charles | 1 | 0 % |
| projectile | 1 | 0 % |
| sole | 1 | 0 % |
| load | 1 | 0 % |
| unique | 1 | 0 % |
| creeping | 1 | 0 % |
| measurement | 1 | 0 % |
| constrained | 1 | 0 % |
| ville | 1 | 0 % |
| projectiles | 1 | 0 % |
| lenght | 1 | 0 % |
| acustica | 1 | 0 % |
| lord | 1 | 0 % |
| stierman | 1 | 0 % |
| gravitation | 1 | 0 % |
| kirschner | 1 | 0 % |
| smooth | 1 | 0 % |
| equilibrium | 1 | 0 % |
| expanding | 1 | 0 % |
| shown | 1 | 0 % |
| yu.n. | 1 | 0 % |
| hannover | 1 | 0 % |
| “partial | 1 | 0 % |
| wind | 1 | 0 % |
| volvo | 1 | 0 % |
| shockwave | 1 | 0 % |
| lj | 1 | 0 % |
| qsou | 1 | 0 % |
| explained | 1 | 0 % |
| modelize | 1 | 0 % |
| exact | 1 | 0 % |
| part | 1 | 0 % |
| argon | 1 | 0 % |
| can | 1 | 0 % |
| algebraic | 1 | 0 % |
| kt | 1 | 0 % |
| shifting | 1 | 0 % |
| lab | 1 | 0 % |
| qian | 1 | 0 % |
| kavitationsblasen | 1 | 0 % |
| euler | 1 | 0 % |
| hardness | 1 | 0 % |
| batchelor | 1 | 0 % |
| nasa | 1 | 0 % |
| gas-liquid | 1 | 0 % |
| visual | 1 | 0 % |
| föttinger | 1 | 0 % |
| circulating | 1 | 0 % |
| astern | 1 | 0 % |
| resonance | 1 | 0 % |
| hydropower | 1 | 0 % |
| runner | 1 | 0 % |
| pcb | 1 | 0 % |
| sheets | 1 | 0 % |
| lezzi | 1 | 0 % |
| c. | 1 | 0 % |
| eng. | 1 | 0 % |
| niclas | 1 | 0 % |
| loaded | 1 | 0 % |
| propulsor | 1 | 0 % |
| flowmeter | 1 | 0 % |
| race | 1 | 0 % |
| explosion | 1 | 0 % |
| steering | 1 | 0 % |
| piping | 1 | 0 % |
| strong | 1 | 0 % |
| convergence | 1 | 0 % |
| boswell | 1 | 0 % |
| naca0015 | 1 | 0 % |
| source | 1 | 0 % |
| measuring | 1 | 0 % |
| tsujimoto | 1 | 0 % |
| transducers | 1 | 0 % |
| lectures/pdf | 1 | 0 % |
| valentine | 1 | 0 % |
| alloy | 1 | 0 % |
| 0020 | 1 | 0 % |
| blunt | 1 | 0 % |
| rupture | 1 | 0 % |
| 1 | 1 | 0 % |
| érosion | 1 | 0 % |
| 144 | 1 | 0 % |
| shuttle | 1 | 0 % |
| chaves | 1 | 0 % |
| blowing | 1 | 0 % |
| price | 1 | 0 % |
| fisheries | 1 | 0 % |
| liquids | 1 | 0 % |
| direct | 1 | 0 % |
| 1973 | 1 | 0 % |
| gary | 1 | 0 % |
| mehmet | 1 | 0 % |
| 32- | 1 | 0 % |
| connected | 1 | 0 % |
| naca0020 | 1 | 0 % |
| gabrielli | 1 | 0 % |
| y | 1 | 0 % |
| dtmb | 1 | 0 % |
| f.r.v | 1 | 0 % |
| throughflow | 1 | 0 % |
| telemetry | 1 | 0 % |
| turbinia | 1 | 0 % |
| quality | 1 | 0 % |
| 1981 | 1 | 0 % |
| akamatsu | 1 | 0 % |
| lecture | 1 | 0 % |
| thèse | 1 | 0 % |
| propcav | 1 | 0 % |
| intensity | 1 | 0 % |
| breakup | 1 | 0 % |
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