| 438 different keywords | Search | Percent |
|---|
| cavitation | 91 | 8.6 % |
| of | 37 | 3.4 % |
| in | 29 | 2.7 % |
| and | 20 | 1.8 % |
| orifice | 17 | 1.6 % |
| a | 16 | 1.5 % |
| supercavitation | 15 | 1.4 % |
| on | 15 | 1.4 % |
| vlsi | 14 | 1.3 % |
| pump | 14 | 1.3 % |
| numerical | 13 | 1.2 % |
| tip | 12 | 1.1 % |
| vortex | 12 | 1.1 % |
| bubble | 11 | 1 % |
| centrifugal | 11 | 1 % |
| the | 10 | 0.9 % |
| simulation | 9 | 0.8 % |
| with | 9 | 0.8 % |
| for | 9 | 0.8 % |
| blades | 8 | 0.7 % |
| experimental | 8 | 0.7 % |
| scale | 7 | 0.6 % |
| 2d-curved | 7 | 0.6 % |
| near | 7 | 0.6 % |
| studies | 7 | 0.6 % |
| effects | 7 | 0.6 % |
| model | 6 | 0.5 % |
| flow | 6 | 0.5 % |
| jet | 6 | 0.5 % |
| rudder | 6 | 0.5 % |
| cav2001 | 6 | 0.5 % |
| boundaries | 5 | 0.4 % |
| b.stoffel | 5 | 0.4 % |
| cavity | 5 | 0.4 % |
| design | 5 | 0.4 % |
| bubbles | 5 | 0.4 % |
| mass | 5 | 0.4 % |
| restriction | 5 | 0.4 % |
| propeller | 5 | 0.4 % |
| m.hoffman | 5 | 0.4 % |
| condition | 5 | 0.4 % |
| jl.reboud | 5 | 0.4 % |
| added | 5 | 0.4 % |
| r.fortes-platella | 5 | 0.4 % |
| kaplan | 5 | 0.4 % |
| cavitating | 5 | 0.4 % |
| o.courier-delgosha | 5 | 0.4 % |
| http | 4 | 0.3 % |
| fluid | 4 | 0.3 % |
| dynamics | 4 | 0.3 % |
| solid | 4 | 0.3 % |
| signal | 4 | 0.3 % |
| tunnel | 4 | 0.3 % |
| behavior | 4 | 0.3 % |
| prediction | 4 | 0.3 % |
| hydrofoil | 4 | 0.3 % |
| system | 3 | 0.2 % |
| pdf | 3 | 0.2 % |
| water | 3 | 0.2 % |
| methods | 3 | 0.2 % |
| two | 3 | 0.2 % |
| analysis | 3 | 0.2 % |
| flows | 3 | 0.2 % |
| erosion | 3 | 0.2 % |
| hydrodynamics | 3 | 0.2 % |
| rotating | 3 | 0.2 % |
| blade | 3 | 0.2 % |
| caltechconf.library.caltech.edu | 3 | 0.2 % |
| effect | 3 | 0.2 % |
| an | 3 | 0.2 % |
| boundary | 3 | 0.2 % |
| hierarchy | 3 | 0.2 % |
| supercavitating | 3 | 0.2 % |
| noise | 3 | 0.2 % |
| measurement | 2 | 0.1 % |
| underwater | 2 | 0.1 % |
| author | 2 | 0.1 % |
| incipient | 2 | 0.1 % |
| disadvantages | 2 | 0.1 % |
| phase | 2 | 0.1 % |
| when | 2 | 0.1 % |
| nand | 2 | 0.1 % |
| experiment | 2 | 0.1 % |
| modeling | 2 | 0.1 % |
| multiphase | 2 | 0.1 % |
| very | 2 | 0.1 % |
| microbubble | 2 | 0.1 % |
| development | 2 | 0.1 % |
| queues | 2 | 0.1 % |
| algorithms | 2 | 0.1 % |
| problem | 2 | 0.1 % |
| c. | 2 | 0.1 % |
| blocks | 2 | 0.1 % |
| single-chip | 2 | 0.1 % |
| integration | 2 | 0.1 % |
| conditions | 2 | 0.1 % |
| supercavitaion | 2 | 0.1 % |
| computers | 2 | 0.1 % |
| physics | 2 | 0.1 % |
| body | 2 | 0.1 % |
| cryogenic | 2 | 0.1 % |
| storage | 2 | 0.1 % |
| behavioural | 2 | 0.1 % |
| takinaci | 2 | 0.1 % |
| new | 2 | 0.1 % |
| strategies | 2 | 0.1 % |
| stress | 2 | 0.1 % |
| models | 2 | 0.1 % |
| algorithm | 2 | 0.1 % |
| pumps | 2 | 0.1 % |
| collapsing | 2 | 0.1 % |
| collapse | 2 | 0.1 % |
| approximation | 2 | 0.1 % |
| unsteady | 2 | 0.1 % |
| dams | 2 | 0.1 % |
| sato | 2 | 0.1 % |
| bart | 2 | 0.1 % |
| //caltechconf.library.caltech.edu/143/1/pope.pdf | 2 | 0.1 % |
| hull | 2 | 0.1 % |
| distribution | 2 | 0.1 % |
| synchronization | 2 | 0.1 % |
| clearance | 2 | 0.1 % |
| is | 2 | 0.1 % |
| rc | 2 | 0.1 % |
| integral | 2 | 0.1 % |
| sheet | 2 | 0.1 % |
| coefficient | 2 | 0.1 % |
| a. | 2 | 0.1 % |
| fission | 2 | 0.1 % |
| building | 2 | 0.1 % |
| fluent | 2 | 0.1 % |
| free | 2 | 0.1 % |
| turbines | 2 | 0.1 % |
| based | 2 | 0.1 % |
| keller | 2 | 0.1 % |
| kawanami | 2 | 0.1 % |
| surge | 2 | 0.1 % |
| locanthi | 2 | 0.1 % |
| developed | 2 | 0.1 % |
| ventilated | 2 | 0.1 % |
| some | 2 | 0.1 % |
| delay | 2 | 0.1 % |
| advantages | 2 | 0.1 % |
| lisp | 2 | 0.1 % |
| rocket | 2 | 0.1 % |
| from | 2 | 0.1 % |
| large | 2 | 0.1 % |
| calculation | 2 | 0.1 % |
| learning | 2 | 0.1 % |
| inception | 2 | 0.1 % |
| leakage | 2 | 0.1 % |
| structure | 2 | 0.1 % |
| slender | 2 | 0.1 % |
| inducer | 1 | 0 % |
| both | 1 | 0 % |
| emu | 1 | 0 % |
| mech | 1 | 0 % |
| projectile | 1 | 0 % |
| implementation | 1 | 0 % |
| code | 1 | 0 % |
| trees | 1 | 0 % |
| visualizations | 1 | 0 % |
| rotation | 1 | 0 % |
| history | 1 | 0 % |
| what | 1 | 0 % |
| elements | 1 | 0 % |
| turbulent | 1 | 0 % |
| re-entrant | 1 | 0 % |
| cal-tech | 1 | 0 % |
| materials | 1 | 0 % |
| emerson | 1 | 0 % |
| concrete | 1 | 0 % |
| computer | 1 | 0 % |
| stimulated | 1 | 0 % |
| naca | 1 | 0 % |
| horn | 1 | 0 % |
| scaling | 1 | 0 % |
| time | 1 | 0 % |
| temperatures | 1 | 0 % |
| strength | 1 | 0 % |
| azipod | 1 | 0 % |
| jets | 1 | 0 % |
| ganippa | 1 | 0 % |
| figures | 1 | 0 % |
| com | 1 | 0 % |
| les | 1 | 0 % |
| review | 1 | 0 % |
| xxx | 1 | 0 % |
| tank | 1 | 0 % |
| circular-cylindrical | 1 | 0 % |
| geometry | 1 | 0 % |
| navier-stokes | 1 | 0 % |
| supercavitation- | 1 | 0 % |
| lagrangian | 1 | 0 % |
| plates | 1 | 0 % |
| cal | 1 | 0 % |
| data | 1 | 0 % |
| sessionb9.005 | 1 | 0 % |
| different | 1 | 0 % |
| computational | 1 | 0 % |
| dmorgan | 1 | 0 % |
| circulation | 1 | 0 % |
| general | 1 | 0 % |
| vibration | 1 | 0 % |
| factor | 1 | 0 % |
| barnaby | 1 | 0 % |
| explain | 1 | 0 % |
| andersson | 1 | 0 % |
| artifical | 1 | 0 % |
| bem | 1 | 0 % |
| combinatorial | 1 | 0 % |
| ductile | 1 | 0 % |
| fully | 1 | 0 % |
| inlet | 1 | 0 % |
| international | 1 | 0 % |
| matuska | 1 | 0 % |
| fully-compressible | 1 | 0 % |
| reinforcement | 1 | 0 % |
| amr | 1 | 0 % |
| content | 1 | 0 % |
| torus | 1 | 0 % |
| discharge | 1 | 0 % |
| gate | 1 | 0 % |
| rate | 1 | 0 % |
| upstream | 1 | 0 % |
| inner | 1 | 0 % |
| drag | 1 | 0 % |
| geometrical | 1 | 0 % |
| hypervelocity | 1 | 0 % |
| problems | 1 | 0 % |
| behaviour | 1 | 0 % |
| video | 1 | 0 % |
| applications | 1 | 0 % |
| kavitation | 1 | 0 % |
| element | 1 | 0 % |
| modified | 1 | 0 % |
| lift | 1 | 0 % |
| -soil | 1 | 0 % |
| naca0015 | 1 | 0 % |
| chapman | 1 | 0 % |
| inst | 1 | 0 % |
| wave | 1 | 0 % |
| mohsen | 1 | 0 % |
| number | 1 | 0 % |
| measuring | 1 | 0 % |
| specific | 1 | 0 % |
| structured | 1 | 0 % |
| section | 1 | 0 % |
| symposium | 1 | 0 % |
| tsujimoto | 1 | 0 % |
| size | 1 | 0 % |
| characteristics | 1 | 0 % |
| journal | 1 | 0 % |
| create | 1 | 0 % |
| chalmer | 1 | 0 % |
| judge | 1 | 0 % |
| japikse | 1 | 0 % |
| single | 1 | 0 % |
| observation | 1 | 0 % |
| tangential | 1 | 0 % |
| surface | 1 | 0 % |
| test | 1 | 0 % |
| advantage | 1 | 0 % |
| instability | 1 | 0 % |
| pipe | 1 | 0 % |
| self | 1 | 0 % |
| artificial | 1 | 0 % |
| j | 1 | 0 % |
| nuclei | 1 | 0 % |
| cloud | 1 | 0 % |
| solving | 1 | 0 % |
| hardware | 1 | 0 % |
| about | 1 | 0 % |
| taylor | 1 | 0 % |
| how | 1 | 0 % |
| similarities | 1 | 0 % |
| reynolds-averaged | 1 | 0 % |
| blowing | 1 | 0 % |
| flat | 1 | 0 % |
| elbow | 1 | 0 % |
| 1991 | 1 | 0 % |
| fourth | 1 | 0 % |
| boundry | 1 | 0 % |
| emission | 1 | 0 % |
| plane | 1 | 0 % |
| 4412 | 1 | 0 % |
| scaled | 1 | 0 % |
| microjet | 1 | 0 % |
| continuous | 1 | 0 % |
| turbulence | 1 | 0 % |
| shaping | 1 | 0 % |
| orfice | 1 | 0 % |
| pressure | 1 | 0 % |
| duke | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| relations | 1 | 0 % |
| liquid | 1 | 0 % |
| thermal | 1 | 0 % |
| due | 1 | 0 % |
| //caltechconf.library.caltech.edu/69/1/anteoncav2001.pdf | 1 | 0 % |
| 2001 | 1 | 0 % |
| ship | 1 | 0 % |
| mccormick | 1 | 0 % |
| savchenko | 1 | 0 % |
| gas | 1 | 0 % |
| found | 1 | 0 % |
| fluids | 1 | 0 % |
| cascade | 1 | 0 % |
| enables | 1 | 0 % |
| throttling | 1 | 0 % |
| cam | 1 | 0 % |
| modelling | 1 | 0 % |
| hovercraft | 1 | 0 % |
| primitives | 1 | 0 % |
| navier | 1 | 0 % |
| length | 1 | 0 % |
| stokes | 1 | 0 % |
| p. | 1 | 0 % |
| two-phase | 1 | 0 % |
| contro; | 1 | 0 % |
| square | 1 | 0 % |
| 2 | 1 | 0 % |
| www.advantages | 1 | 0 % |
| requirement | 1 | 0 % |
| absrtact | 1 | 0 % |
| similar | 1 | 0 % |
| hydrofoils | 1 | 0 % |
| timed | 1 | 0 % |
| acosta | 1 | 0 % |
| lumley | 1 | 0 % |
| stream | 1 | 0 % |
| torpedoes | 1 | 0 % |
| overview | 1 | 0 % |
| cav | 1 | 0 % |
| hydrodynamic | 1 | 0 % |
| unstable | 1 | 0 % |
| filetype | 1 | 0 % |
| kanazawa | 1 | 0 % |
| partial | 1 | 0 % |
| suction | 1 | 0 % |
| instabilities | 1 | 0 % |
| limit | 1 | 0 % |
| torpedo | 1 | 0 % |
| networks. | 1 | 0 % |
| boat | 1 | 0 % |
| localized | 1 | 0 % |
| bearings | 1 | 0 % |
| transistor | 1 | 0 % |
| a-10 | 1 | 0 % |
| through | 1 | 0 % |
| periodicity | 1 | 0 % |
| foil | 1 | 0 % |
| testing | 1 | 0 % |
| around | 1 | 0 % |
| plesset | 1 | 0 % |
| empirically | 1 | 0 % |
| sensor | 1 | 0 % |
| that | 1 | 0 % |
| attenuation | 1 | 0 % |
| layout | 1 | 0 % |
| hydraulic | 1 | 0 % |
| //caltechconf.library.caltech.edu/175/1/amrmohsen.pdf | 1 | 0 % |
| keiichi | 1 | 0 % |
| 2d | 1 | 0 % |
| massaij | 1 | 0 % |
| transition | 1 | 0 % |
| tiling | 1 | 0 % |
| inducers | 1 | 0 % |
| hydroplane | 1 | 0 % |
| pates | 1 | 0 % |
| cellular | 1 | 0 % |
| simple | 1 | 0 % |
| saito | 1 | 0 % |
| vehicle | 1 | 0 % |
| supercavity | 1 | 0 % |
| goes | 1 | 0 % |
| range | 1 | 0 % |
| motor | 1 | 0 % |
| velocity | 1 | 0 % |
| icdl | 1 | 0 % |
| sizing | 1 | 0 % |
| architecture | 1 | 0 % |
| to | 1 | 0 % |
| spectrometer | 1 | 0 % |
| alpha | 1 | 0 % |
| motion | 1 | 0 % |
| averaged | 1 | 0 % |
| root | 1 | 0 % |
| method | 1 | 0 % |
| hierarchial | 1 | 0 % |
| radiated | 1 | 0 % |
| language | 1 | 0 % |
| trajectory | 1 | 0 % |
| any | 1 | 0 % |
| chomiak | 1 | 0 % |
| 1/6 | 1 | 0 % |
| nozzle | 1 | 0 % |
| wake | 1 | 0 % |
| material | 1 | 0 % |
| david | 1 | 0 % |
| priority | 1 | 0 % |
| investigations | 1 | 0 % |
| bark | 1 | 0 % |
| frequency | 1 | 0 % |
| perspective | 1 | 0 % |
| directed | 1 | 0 % |
| does | 1 | 0 % |
| brennen | 1 | 0 % |
| location | 1 | 0 % |
| meant | 1 | 0 % |
| high-speed | 1 | 0 % |
| geometrically | 1 | 0 % |
| logical | 1 | 0 % |
| calculate | 1 | 0 % |
| leading | 1 | 0 % |
| theory | 1 | 0 % |
| zhong | 1 | 0 % |
| indication | 1 | 0 % |
| abstract | 1 | 0 % |
| management | 1 | 0 % |
| types | 1 | 0 % |
| interaction | 1 | 0 % |
| purpose | 1 | 0 % |
| boundaries. | 1 | 0 % |
| are | 1 | 0 % |
| straight | 1 | 0 % |
| at | 1 | 0 % |
| physical | 1 | 0 % |
| edge | 1 | 0 % |
| towing | 1 | 0 % |
| cq | 1 | 0 % |
| thin | 1 | 0 % |
| 3 | 1 | 0 % |
| flow. | 1 | 0 % |
| wavelet | 1 | 0 % |
| calculation. | 1 | 0 % |
| experiments | 1 | 0 % |
| air | 1 | 0 % |
|