| 924 different keywords | Search | Percent |
|---|
| cavitation | 326 | 8.7 % |
| of | 165 | 4.4 % |
| orifice | 108 | 2.8 % |
| in | 81 | 2.1 % |
| and | 75 | 2 % |
| a | 63 | 1.6 % |
| restriction | 62 | 1.6 % |
| pump | 59 | 1.5 % |
| on | 57 | 1.5 % |
| vortex | 51 | 1.3 % |
| flow | 49 | 1.3 % |
| the | 36 | 0.9 % |
| propeller | 34 | 0.9 % |
| erosion | 34 | 0.9 % |
| bubble | 32 | 0.8 % |
| pdf | 31 | 0.8 % |
| water | 29 | 0.7 % |
| supercavitation | 28 | 0.7 % |
| model | 27 | 0.7 % |
| plate | 26 | 0.6 % |
| noise | 25 | 0.6 % |
| for | 24 | 0.6 % |
| experimental | 24 | 0.6 % |
| numerical | 23 | 0.6 % |
| analysis | 23 | 0.6 % |
| centrifugal | 21 | 0.5 % |
| simulation | 19 | 0.5 % |
| study | 18 | 0.4 % |
| number | 17 | 0.4 % |
| quality | 17 | 0.4 % |
| tip | 17 | 0.4 % |
| with | 17 | 0.4 % |
| speed | 17 | 0.4 % |
| design | 17 | 0.4 % |
| mass | 16 | 0.4 % |
| cfd | 16 | 0.4 % |
| fluent | 16 | 0.4 % |
| dynamics | 15 | 0.4 % |
| pressure | 15 | 0.4 % |
| filetype | 15 | 0.4 % |
| international | 15 | 0.4 % |
| paper | 14 | 0.3 % |
| ventilated | 14 | 0.3 % |
| added | 14 | 0.3 % |
| to | 14 | 0.3 % |
| rocket | 14 | 0.3 % |
| calculation | 13 | 0.3 % |
| symposium | 12 | 0.3 % |
| pipe | 12 | 0.3 % |
| suction | 12 | 0.3 % |
| effect | 12 | 0.3 % |
| flows | 11 | 0.2 % |
| hydrofoil | 11 | 0.2 % |
| cavities | 11 | 0.2 % |
| diesel | 11 | 0.2 % |
| instabilities | 11 | 0.2 % |
| azipod | 10 | 0.2 % |
| experiment | 10 | 0.2 % |
| test | 10 | 0.2 % |
| mesh | 10 | 0.2 % |
| jet | 10 | 0.2 % |
| is | 10 | 0.2 % |
| sheet | 10 | 0.2 % |
| effects | 10 | 0.2 % |
| super | 9 | 0.2 % |
| surface | 9 | 0.2 % |
| template | 9 | 0.2 % |
| inducer | 9 | 0.2 % |
| pumps | 9 | 0.2 % |
| valve | 9 | 0.2 % |
| partial | 9 | 0.2 % |
| from | 9 | 0.2 % |
| kaplan | 9 | 0.2 % |
| fluid | 8 | 0.2 % |
| turbine | 8 | 0.2 % |
| velocity | 8 | 0.2 % |
| supercavitating | 8 | 0.2 % |
| cavitating | 8 | 0.2 % |
| cav2001 | 8 | 0.2 % |
| impeller | 8 | 0.2 % |
| tab_hty | 8 | 0.2 % |
| turbo | 8 | 0.2 % |
| hydraulic | 8 | 0.2 % |
| near | 8 | 0.2 % |
| bubbles | 7 | 0.1 % |
| technical | 7 | 0.1 % |
| liquid | 7 | 0.1 % |
| sound | 7 | 0.1 % |
| cascade | 7 | 0.1 % |
| pitching | 7 | 0.1 % |
| hydrofoils | 7 | 0.1 % |
| sae | 7 | 0.1 % |
| between | 7 | 0.1 % |
| modeling | 7 | 0.1 % |
| mechanism | 7 | 0.1 % |
| wave | 7 | 0.1 % |
| tunnel | 7 | 0.1 % |
| cloud | 7 | 0.1 % |
| damping | 7 | 0.1 % |
| gas | 7 | 0.1 % |
| equation | 7 | 0.1 % |
| rudder | 7 | 0.1 % |
| submerged | 7 | 0.1 % |
| nexearch | 7 | 0.1 % |
| measurement | 6 | 0.1 % |
| plates | 6 | 0.1 % |
| how | 6 | 0.1 % |
| collapse | 6 | 0.1 % |
| emission | 6 | 0.1 % |
| unsteady | 6 | 0.1 % |
| acoustic | 6 | 0.1 % |
| low | 6 | 0.1 % |
| experiments | 6 | 0.1 % |
| cavity | 6 | 0.1 % |
| characteristics | 6 | 0.1 % |
| dynamic | 6 | 0.1 % |
| orifices | 6 | 0.1 % |
| joint | 6 | 0.1 % |
| nozzle | 6 | 0.1 % |
| high | 6 | 0.1 % |
| what | 5 | 0.1 % |
| turbopump | 5 | 0.1 % |
| by | 5 | 0.1 % |
| note | 5 | 0.1 % |
| intake | 5 | 0.1 % |
| flat | 5 | 0.1 % |
| pipes | 5 | 0.1 % |
| length | 5 | 0.1 % |
| butterfly | 5 | 0.1 % |
| singhal | 5 | 0.1 % |
| interaction | 5 | 0.1 % |
| tullis | 5 | 0.1 % |
| boundaries | 5 | 0.1 % |
| turbulent | 5 | 0.1 % |
| prediction | 5 | 0.1 % |
| ship | 5 | 0.1 % |
| forces | 5 | 0.1 % |
| s | 5 | 0.1 % |
| installation | 5 | 0.1 % |
| frequency | 5 | 0.1 % |
| at | 5 | 0.1 % |
| leakage | 5 | 0.1 % |
| materials | 4 | 0.1 % |
| phase | 4 | 0.1 % |
| type | 4 | 0.1 % |
| vortices | 4 | 0.1 % |
| video | 4 | 0.1 % |
| axial | 4 | 0.1 % |
| oscillation | 4 | 0.1 % |
| performance | 4 | 0.1 % |
| 2001 | 4 | 0.1 % |
| distribution | 4 | 0.1 % |
| cavitator | 4 | 0.1 % |
| two-phase | 4 | 0.1 % |
| rotating | 4 | 0.1 % |
| blade | 4 | 0.1 % |
| impact | 4 | 0.1 % |
| that | 4 | 0.1 % |
| layer | 4 | 0.1 % |
| time-frequency | 4 | 0.1 % |
| boundary | 4 | 0.1 % |
| engine | 4 | 0.1 % |
| types | 4 | 0.1 % |
| research | 4 | 0.1 % |
| . | 4 | 0.1 % |
| naca | 4 | 0.1 % |
| generation | 4 | 0.1 % |
| systems | 4 | 0.1 % |
| injection | 4 | 0.1 % |
| propellers | 4 | 0.1 % |
| tanguay | 4 | 0.1 % |
| shock | 4 | 0.1 % |
| size | 4 | 0.1 % |
| using | 4 | 0.1 % |
| methods | 4 | 0.1 % |
| fourth | 4 | 0.1 % |
| blades | 4 | 0.1 % |
| two | 4 | 0.1 % |
| generator | 4 | 0.1 % |
| mixed | 4 | 0.1 % |
| method | 4 | 0.1 % |
| abstract | 4 | 0.1 % |
| horn | 3 | 0 % |
| when | 3 | 0 % |
| coefficients | 3 | 0 % |
| re | 3 | 0 % |
| 2-d | 3 | 0 % |
| caltech | 3 | 0 % |
| ductile | 3 | 0 % |
| inlet | 3 | 0 % |
| gate | 3 | 0 % |
| piping | 3 | 0 % |
| front | 3 | 0 % |
| 12 | 3 | 0 % |
| facing | 3 | 0 % |
| step | 3 | 0 % |
| entrant | 3 | 0 % |
| injectors | 3 | 0 % |
| related | 3 | 0 % |
| g. | 3 | 0 % |
| coefficient | 3 | 0 % |
| asme | 3 | 0 % |
| theoretical | 3 | 0 % |
| its | 3 | 0 % |
| inducers | 3 | 0 % |
| 20-23 | 3 | 0 % |
| measurements | 3 | 0 % |
| lithotripsy | 3 | 0 % |
| an | 3 | 0 % |
| turbomachinery | 3 | 0 % |
| transitional | 3 | 0 % |
| intakes | 3 | 0 % |
| june | 3 | 0 % |
| phenomenon | 3 | 0 % |
| code | 3 | 0 % |
| history | 3 | 0 % |
| j. | 3 | 0 % |
| comparison | 3 | 0 % |
| - | 3 | 0 % |
| geometry | 3 | 0 % |
| data | 3 | 0 % |
| senocak | 3 | 0 % |
| vibration | 3 | 0 % |
| mechanisms | 3 | 0 % |
| third | 3 | 0 % |
| has | 3 | 0 % |
| discharge | 3 | 0 % |
| upstream | 3 | 0 % |
| problems | 3 | 0 % |
| applications | 3 | 0 % |
| abs | 3 | 0 % |
| cryogenic | 3 | 0 % |
| meter | 3 | 0 % |
| approach | 3 | 0 % |
| cavitaion | 3 | 0 % |
| downstream | 3 | 0 % |
| reference | 3 | 0 % |
| backward | 3 | 0 % |
| abstracts | 3 | 0 % |
| h. | 3 | 0 % |
| if | 3 | 0 % |
| conference | 3 | 0 % |
| investigation | 3 | 0 % |
| i | 3 | 0 % |
| characteristic | 3 | 0 % |
| michel | 3 | 0 % |
| rayleigh | 3 | 0 % |
| diameter | 3 | 0 % |
| piercing | 3 | 0 % |
| mach | 2 | 0 % |
| projectile | 2 | 0 % |
| finite | 2 | 0 % |
| constrained | 2 | 0 % |
| equilibrium | 2 | 0 % |
| shown | 2 | 0 % |
| incipient | 2 | 0 % |
| supercavities | 2 | 0 % |
| sauer | 2 | 0 % |
| proposal | 2 | 0 % |
| walls | 2 | 0 % |
| mixtrue | 2 | 0 % |
| very | 2 | 0 % |
| may | 2 | 0 % |
| runner | 2 | 0 % |
| trailing | 2 | 0 % |
| proceedings | 2 | 0 % |
| solid | 2 | 0 % |
| flowmeter | 2 | 0 % |
| rate | 2 | 0 % |
| perspectives | 2 | 0 % |
| conditions | 2 | 0 % |
| injector | 2 | 0 % |
| journal | 2 | 0 % |
| ratio | 2 | 0 % |
| observation | 2 | 0 % |
| rupture | 2 | 0 % |
| ittc | 2 | 0 % |
| instability | 2 | 0 % |
| pitch | 2 | 0 % |
| scale | 2 | 0 % |
| best | 2 | 0 % |
| even | 2 | 0 % |
| elbow | 2 | 0 % |
| behavior | 2 | 0 % |
| format | 2 | 0 % |
| photo | 2 | 0 % |
| relations | 2 | 0 % |
| & | 2 | 0 % |
| formula | 2 | 0 % |
| errosion | 2 | 0 % |
| sump | 2 | 0 % |
| ps | 2 | 0 % |
| download | 2 | 0 % |
| small | 2 | 0 % |
| found | 2 | 0 % |
| fluids | 2 | 0 % |
| next | 2 | 0 % |
| stokes | 2 | 0 % |
| valves | 2 | 0 % |
| changes | 2 | 0 % |
| hydrodynamic | 2 | 0 % |
| compressors | 2 | 0 % |
| turbines | 2 | 0 % |
| fluctuation | 2 | 0 % |
| foil | 2 | 0 % |
| distance | 2 | 0 % |
| empirically | 2 | 0 % |
| breakoff | 2 | 0 % |
| wärme | 2 | 0 % |
| tab_hty.top | 2 | 0 % |
| overlapping | 2 | 0 % |
| saito | 2 | 0 % |
| some | 2 | 0 % |
| detection | 2 | 0 % |
| sizing | 2 | 0 % |
| claude | 2 | 0 % |
| real | 2 | 0 % |
| shoc | 2 | 0 % |
| trajectory | 2 | 0 % |
| provided | 2 | 0 % |
| techniques | 2 | 0 % |
| shockwaves | 2 | 0 % |
| inflow | 2 | 0 % |
| wake | 2 | 0 % |
| vessel | 2 | 0 % |
| filetype%3apdf | 2 | 0 % |
| bark | 2 | 0 % |
| interface | 2 | 0 % |
| rebattet | 2 | 0 % |
| s. | 2 | 0 % |
| microbubbles | 2 | 0 % |
| center | 2 | 0 % |
| symp. | 2 | 0 % |
| inside | 2 | 0 % |
| physical | 2 | 0 % |
| edge | 2 | 0 % |
| working | 2 | 0 % |
| application | 2 | 0 % |
| force | 2 | 0 % |
| vortexing | 2 | 0 % |
| passage | 2 | 0 % |
| numeca | 2 | 0 % |
| reduction | 2 | 0 % |
| time | 2 | 0 % |
| nozzles | 2 | 0 % |
| sumps | 2 | 0 % |
| rapidly | 2 | 0 % |
| rebound | 2 | 0 % |
| turbopumps | 2 | 0 % |
| remove | 2 | 0 % |
| bellmouth | 2 | 0 % |
| mixture | 2 | 0 % |
| 1962 | 2 | 0 % |
| zamm | 2 | 0 % |
| wagner | 2 | 0 % |
| maximum | 2 | 0 % |
| kunz | 2 | 0 % |
| impellers | 2 | 0 % |
| factor | 2 | 0 % |
| control | 2 | 0 % |
| closed | 2 | 0 % |
| bem | 2 | 0 % |
| apparatus | 2 | 0 % |
| pits | 2 | 0 % |
| engineering | 2 | 0 % |
| effects. | 2 | 0 % |
| enough. | 2 | 0 % |
| laser-induced | 2 | 0 % |
| hole | 2 | 0 % |
| singularity | 2 | 0 % |
| 1996 | 2 | 0 % |
| compressibility | 2 | 0 % |
| cavitation-vortex | 2 | 0 % |
| occurred | 2 | 0 % |
| transient | 2 | 0 % |
| numercial | 2 | 0 % |
| use | 2 | 0 % |
| orrifice | 2 | 0 % |
| sato | 2 | 0 % |
| steel | 2 | 0 % |
| conclusion | 2 | 0 % |
| throttling | 2 | 0 % |
| shyy | 2 | 0 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 2 | 0 % |
| modelling | 2 | 0 % |
| schnerr | 2 | 0 % |
| helium | 2 | 0 % |
| supercavitatioin | 2 | 0 % |
| chromebar | 2 | 0 % |
| induced | 2 | 0 % |
| cav | 2 | 0 % |
| fifth | 2 | 0 % |
| around | 2 | 0 % |
| phenomena | 2 | 0 % |
| 2d | 2 | 0 % |
| cavitations | 2 | 0 % |
| simple | 2 | 0 % |
| efficiency | 2 | 0 % |
| burgers | 2 | 0 % |
| dominate | 2 | 0 % |
| homogeneous | 2 | 0 % |
| media | 2 | 0 % |
| lifting | 2 | 0 % |
| song | 2 | 0 % |
| calculate | 2 | 0 % |
| barotropic | 2 | 0 % |
| transparent | 2 | 0 % |
| f | 2 | 0 % |
| epfl | 2 | 0 % |
| stop | 2 | 0 % |
| air | 2 | 0 % |
| spl | 1 | 0 % |
| modle | 1 | 0 % |
| caviation | 1 | 0 % |
| opening | 1 | 0 % |
| issue | 1 | 0 % |
| particle | 1 | 0 % |
| shapes | 1 | 0 % |
| âcavus | 1 | 0 % |
| light | 1 | 0 % |
| lord | 1 | 0 % |
| underwater | 1 | 0 % |
| used | 1 | 0 % |
| diamter | 1 | 0 % |
| sizer | 1 | 0 % |
| scaling | 1 | 0 % |
| tomita | 1 | 0 % |
| system | 1 | 0 % |
| wall | 1 | 0 % |
| thermodynamic | 1 | 0 % |
| turning | 1 | 0 % |
| factor%2bhow | 1 | 0 % |
| 4th | 1 | 0 % |
| marine | 1 | 0 % |
| ikohagi | 1 | 0 % |
| nurick | 1 | 0 % |
| vessels | 1 | 0 % |
| philipp | 1 | 0 % |
| froude | 1 | 0 % |
| can | 1 | 0 % |
| 15 | 1 | 0 % |
| henrik | 1 | 0 % |
| derived | 1 | 0 % |
| prop | 1 | 0 % |
| average | 1 | 0 % |
| star-cd | 1 | 0 % |
| t. | 1 | 0 % |
| helical | 1 | 0 % |
| static | 1 | 0 % |
| m2 | 1 | 0 % |
| rf | 1 | 0 % |
| joints | 1 | 0 % |
| cause | 1 | 0 % |
| navier-stokes | 1 | 0 % |
| lda | 1 | 0 % |
| tech | 1 | 0 % |
| flange? | 1 | 0 % |
| different | 1 | 0 % |
| vertical | 1 | 0 % |
| computational | 1 | 0 % |
| inch | 1 | 0 % |
| bteween | 1 | 0 % |
| sweep | 1 | 0 % |
| h.; | 1 | 0 % |
| installed | 1 | 0 % |
| industrial | 1 | 0 % |
| mid | 1 | 0 % |
| plessett | 1 | 0 % |
| moving | 1 | 0 % |
| expriment | 1 | 0 % |
| fatigue | 1 | 0 % |
| denmark | 1 | 0 % |
| mech. | 1 | 0 % |
| produced | 1 | 0 % |
| thakur | 1 | 0 % |
| heat | 1 | 0 % |
| vibratory | 1 | 0 % |
| there | 1 | 0 % |
| heave | 1 | 0 % |
| quick | 1 | 0 % |
| attainable | 1 | 0 % |
| equations | 1 | 0 % |
| 1995. | 1 | 0 % |
| tables | 1 | 0 % |
| ordering | 1 | 0 % |
| cawitation | 1 | 0 % |
| drag | 1 | 0 % |
| leroux | 1 | 0 % |
| affect | 1 | 0 % |
| kavitation | 1 | 0 % |
| -umâ | 1 | 0 % |
| fedsm99-7364 | 1 | 0 % |
| equipment | 1 | 0 % |
| i. | 1 | 0 % |
| 113 | 1 | 0 % |
| protection | 1 | 0 % |
| submergence | 1 | 0 % |
| measuring | 1 | 0 % |
| processes | 1 | 0 % |
| series | 1 | 0 % |
| 87 | 1 | 0 % |
| 1.0mpa | 1 | 0 % |
| multi-cavitation | 1 | 0 % |
| mouth | 1 | 0 % |
| called | 1 | 0 % |
| alloy | 1 | 0 % |
| supersonic | 1 | 0 % |
| 0012 | 1 | 0 % |
| artificial | 1 | 0 % |
| state | 1 | 0 % |
| multi-hole | 1 | 0 % |
| mcnown | 1 | 0 % |
| about | 1 | 0 % |
| designing | 1 | 0 % |
| drift | 1 | 0 % |
| crack | 1 | 0 % |
| models | 1 | 0 % |
| 120 | 1 | 0 % |
| similarities | 1 | 0 % |
| event | 1 | 0 % |
| bell | 1 | 0 % |
| tunnels | 1 | 0 % |
| pd | 1 | 0 % |
| relation | 1 | 0 % |
| creating | 1 | 0 % |
| hydrofoil. | 1 | 0 % |
| liquids | 1 | 0 % |
| chart | 1 | 0 % |
| jp | 1 | 0 % |
| cl | 1 | 0 % |
| uncertainty | 1 | 0 % |
| rules | 1 | 0 % |
| sheet/cloud | 1 | 0 % |
| chyczewski | 1 | 0 % |
| s15c | 1 | 0 % |
| bodies | 1 | 0 % |
| should | 1 | 0 % |
| approximation | 1 | 0 % |
| throttleing | 1 | 0 % |
| spitzenwirbel | 1 | 0 % |
| fresh | 1 | 0 % |
| naca0020 | 1 | 0 % |
| point | 1 | 0 % |
| charactertistics | 1 | 0 % |
| kyowaãpgm-2kc | 1 | 0 % |
| facilities | 1 | 0 % |
| surface. | 1 | 0 % |
| nozzlehole | 1 | 0 % |
| eulerian | 1 | 0 % |
| elimination | 1 | 0 % |
| da | 1 | 0 % |
| orificemeter | 1 | 0 % |
| y | 1 | 0 % |
| reentrant | 1 | 0 % |
| lohrberg | 1 | 0 % |
| isaãcavitation | 1 | 0 % |
| cone | 1 | 0 % |
| hull | 1 | 0 % |
| turbomachine | 1 | 0 % |
| mccormick | 1 | 0 % |
| âcalculation | 1 | 0 % |
| sg6 | 1 | 0 % |
| savchenko | 1 | 0 % |
| w | 1 | 0 % |
| spectral | 1 | 0 % |
| cavitation%2c | 1 | 0 % |
| over | 1 | 0 % |
| centrifugal%2cpdf | 1 | 0 % |
| visualization | 1 | 0 % |
| enviromental | 1 | 0 % |
| naval | 1 | 0 % |
| schall | 1 | 0 % |
| akamatsu | 1 | 0 % |
| chayut | 1 | 0 % |
| instead | 1 | 0 % |
| online | 1 | 0 % |
| astm | 1 | 0 % |
| multi-phase | 1 | 0 % |
| concepts | 1 | 0 % |
| troubleshoot | 1 | 0 % |
| intensity | 1 | 0 % |
| 1980 | 1 | 0 % |
| law | 1 | 0 % |
| oti | 1 | 0 % |
| square | 1 | 0 % |
| off | 1 | 0 % |
| staging | 1 | 0 % |
| like | 1 | 0 % |
| tu | 1 | 0 % |
| approximately | 1 | 0 % |
| h1 | 1 | 0 % |
| parameters | 1 | 0 % |
| pressurepulses | 1 | 0 % |
| word | 1 | 0 % |
| nm | 1 | 0 % |
| unstable | 1 | 0 % |
| xiaolangdi | 1 | 0 % |
| position | 1 | 0 % |
| tainter | 1 | 0 % |
| dr. | 1 | 0 % |
| planing | 1 | 0 % |
| restricting | 1 | 0 % |
| scale-up | 1 | 0 % |
| tanks | 1 | 0 % |
| specification | 1 | 0 % |
| free | 1 | 0 % |
| features | 1 | 0 % |
| m | 1 | 0 % |
| across | 1 | 0 % |
| oil | 1 | 0 % |
| through | 1 | 0 % |
| hattori | 1 | 0 % |
| explanation | 1 | 0 % |
| jousselin | 1 | 0 % |
| flows. | 1 | 0 % |
| okada | 1 | 0 % |
| lochscheiben | 1 | 0 % |
| boger | 1 | 0 % |
| molecular | 1 | 0 % |
| table | 1 | 0 % |
| takemura | 1 | 0 % |
| tool | 1 | 0 % |
| jsme | 1 | 0 % |
| runge | 1 | 0 % |
| based | 1 | 0 % |
| loading | 1 | 0 % |
| similarity | 1 | 0 % |
| acqusition | 1 | 0 % |
| 1.5 | 1 | 0 % |
| mushroom | 1 | 0 % |
| goltz | 1 | 0 % |
| pulse | 1 | 0 % |
| linear | 1 | 0 % |
| solution | 1 | 0 % |
| sphericity | 1 | 0 % |
| transfer | 1 | 0 % |
| motion | 1 | 0 % |
| angle | 1 | 0 % |
| frv | 1 | 0 % |
| device | 1 | 0 % |
| correcting | 1 | 0 % |
| Ä°n | 1 | 0 % |
| hydro | 1 | 0 % |
| merkle | 1 | 0 % |
| investigations | 1 | 0 % |
| bands | 1 | 0 % |
| vavle | 1 | 0 % |
| orifis | 1 | 0 % |
| field | 1 | 0 % |
| 310 | 1 | 0 % |
| treatment | 1 | 0 % |
| strain | 1 | 0 % |
| shape | 1 | 0 % |
| tracking | 1 | 0 % |
| bodies. | 1 | 0 % |
| xxxxxxx | 1 | 0 % |
| lump | 1 | 0 % |
| disk | 1 | 0 % |
| degree | 1 | 0 % |
| purpose | 1 | 0 % |
| equivalent | 1 | 0 % |
| young | 1 | 0 % |
| propoller | 1 | 0 % |
| cavâ95 | 1 | 0 % |
| spiral | 1 | 0 % |
| thornycroft | 1 | 0 % |
| breakdown | 1 | 0 % |
| example | 1 | 0 % |
| photographs | 1 | 0 % |
| reboud | 1 | 0 % |
| space | 1 | 0 % |
| vs | 1 | 0 % |
| book | 1 | 0 % |
| pictures | 1 | 0 % |
| initial | 1 | 0 % |
| 3d | 1 | 0 % |
| program | 1 | 0 % |
| fision | 1 | 0 % |
| jj | 1 | 0 % |
| npsh | 1 | 0 % |
| lengths | 1 | 0 % |
| tutorials | 1 | 0 % |
| chamber | 1 | 0 % |
| sceintific | 1 | 0 % |
| re-entrant | 1 | 0 % |
| rotate | 1 | 0 % |
| orifice.pdf | 1 | 0 % |
| watanab.t | 1 | 0 % |
| vladimir | 1 | 0 % |
| maintain | 1 | 0 % |
| flashing | 1 | 0 % |
| round | 1 | 0 % |
| pumo | 1 | 0 % |
| inlet#sclient=psy-ab | 1 | 0 % |
| %2c1980 | 1 | 0 % |
| jens | 1 | 0 % |
| levels | 1 | 0 % |
| concentration | 1 | 0 % |
| fft | 1 | 0 % |
| 1948 | 1 | 0 % |
| thesis | 1 | 0 % |
| review | 1 | 0 % |
| narrow | 1 | 0 % |
| vapo | 1 | 0 % |
| wh | 1 | 0 % |
| single-phase | 1 | 0 % |
| multiphase | 1 | 0 % |
| following | 1 | 0 % |
| lagrangian | 1 | 0 % |
| salt | 1 | 0 % |
| diagram | 1 | 0 % |
| cal | 1 | 0 % |
| 0015 | 1 | 0 % |
| stable | 1 | 0 % |
| shedding | 1 | 0 % |
| spherical | 1 | 0 % |
| restrict | 1 | 0 % |
| âhollowâ | 1 | 0 % |
| barnaby | 1 | 0 % |
| erosive | 1 | 0 % |
| hj. | 1 | 0 % |
| rhr | 1 | 0 % |
| flexible | 1 | 0 % |
| cd | 1 | 0 % |
| nuntadusit | 1 | 0 % |
| boncinelli | 1 | 0 % |
| gradient | 1 | 0 % |
| pattern | 1 | 0 % |
| as | 1 | 0 % |
| fully | 1 | 0 % |
| 5 | 1 | 0 % |
| kato | 1 | 0 % |
| d | 1 | 0 % |
| theoretically | 1 | 0 % |
| cutaway | 1 | 0 % |
| maneuvering | 1 | 0 % |
| break | 1 | 0 % |
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