| 328 different keywords | Search | Percent |
|---|
| cavitation | 48 | 6.2 % |
| of | 32 | 4.1 % |
| mos | 25 | 3.2 % |
| flip | 16 | 2 % |
| and | 16 | 2 % |
| in | 14 | 1.8 % |
| bubble | 14 | 1.8 % |
| numerical | 12 | 1.5 % |
| supercavitation | 12 | 1.5 % |
| vortex | 12 | 1.5 % |
| flop | 11 | 1.4 % |
| a | 9 | 1.1 % |
| simulation | 9 | 1.1 % |
| vlsi | 9 | 1.1 % |
| http | 7 | 0.9 % |
| flipflop | 7 | 0.9 % |
| cavity | 7 | 0.9 % |
| flow | 7 | 0.9 % |
| //caltechconf.library.caltech.edu/209/ | 7 | 0.9 % |
| model | 6 | 0.7 % |
| on | 6 | 0.7 % |
| design | 6 | 0.7 % |
| pump | 6 | 0.7 % |
| for | 6 | 0.7 % |
| cavitating | 6 | 0.7 % |
| the | 5 | 0.6 % |
| flops | 5 | 0.6 % |
| what | 4 | 0.5 % |
| re-entrant | 4 | 0.5 % |
| supersonic | 4 | 0.5 % |
| jet | 4 | 0.5 % |
| propeller | 4 | 0.5 % |
| is | 4 | 0.5 % |
| flows | 4 | 0.5 % |
| cascade | 4 | 0.5 % |
| acoustic | 4 | 0.5 % |
| partial | 4 | 0.5 % |
| instabilities | 4 | 0.5 % |
| hydrofoil | 4 | 0.5 % |
| with | 4 | 0.5 % |
| nozzle | 4 | 0.5 % |
| centrifugal | 4 | 0.5 % |
| super | 3 | 0.3 % |
| modeling | 3 | 0.3 % |
| blocks | 3 | 0.3 % |
| wave | 3 | 0.3 % |
| ring | 3 | 0.3 % |
| scale | 3 | 0.3 % |
| collapse | 3 | 0.3 % |
| orifice | 3 | 0.3 % |
| morel | 3 | 0.3 % |
| damping | 3 | 0.3 % |
| erosion | 3 | 0.3 % |
| p. | 3 | 0.3 % |
| a. | 3 | 0.3 % |
| philippe | 3 | 0.3 % |
| keller | 3 | 0.3 % |
| ventilated | 3 | 0.3 % |
| to | 3 | 0.3 % |
| kaplan | 3 | 0.3 % |
| inception | 3 | 0.3 % |
| effects | 3 | 0.3 % |
| circuits | 2 | 0.2 % |
| martin | 2 | 0.2 % |
| cleaver | 2 | 0.2 % |
| turbulent | 2 | 0.2 % |
| j. | 2 | 0.2 % |
| underwater | 2 | 0.2 % |
| emerson | 2 | 0.2 % |
| turbopump | 2 | 0.2 % |
| nozzles | 2 | 0.2 % |
| schaffar | 2 | 0.2 % |
| prop | 2 | 0.2 % |
| pdf | 2 | 0.2 % |
| limitation | 2 | 0.2 % |
| object | 2 | 0.2 % |
| industrial | 2 | 0.2 % |
| photographic | 2 | 0.2 % |
| water | 2 | 0.2 % |
| solid | 2 | 0.2 % |
| diaphragm | 2 | 0.2 % |
| processor | 2 | 0.2 % |
| clark | 2 | 0.2 % |
| discrete | 2 | 0.2 % |
| thompson | 2 | 0.2 % |
| p.antognetti | 2 | 0.2 % |
| cabitation | 2 | 0.2 % |
| intake | 2 | 0.2 % |
| single | 2 | 0.2 % |
| tunnel | 2 | 0.2 % |
| y.tsividis | 2 | 0.2 % |
| pipe | 2 | 0.2 % |
| advantage | 2 | 0.2 % |
| casio | 2 | 0.2 % |
| communications | 2 | 0.2 % |
| complexity | 2 | 0.2 % |
| cavities | 2 | 0.2 % |
| emission | 2 | 0.2 % |
| unsteady | 2 | 0.2 % |
| thermal | 2 | 0.2 % |
| 2001 | 2 | 0.2 % |
| analysis | 2 | 0.2 % |
| ship | 2 | 0.2 % |
| transform | 2 | 0.2 % |
| sheet | 2 | 0.2 % |
| turbine | 2 | 0.2 % |
| cfd | 2 | 0.2 % |
| stream | 2 | 0.2 % |
| induced | 2 | 0.2 % |
| cav | 2 | 0.2 % |
| oc-g1000 | 2 | 0.2 % |
| hydrodynamic | 2 | 0.2 % |
| fluent | 2 | 0.2 % |
| macintyre | 2 | 0.2 % |
| suction | 2 | 0.2 % |
| interact | 2 | 0.2 % |
| tip | 2 | 0.2 % |
| spectrometer | 2 | 0.2 % |
| 2015 | 2 | 0.2 % |
| bristle | 2 | 0.2 % |
| field | 2 | 0.2 % |
| supercavitating | 2 | 0.2 % |
| experimental | 2 | 0.2 % |
| usage | 2 | 0.2 % |
| wavelet | 2 | 0.2 % |
| closure | 1 | 0.1 % |
| n. | 1 | 0.1 % |
| stall | 1 | 0.1 % |
| history | 1 | 0.1 % |
| projectiles | 1 | 0.1 % |
| optimal | 1 | 0.1 % |
| waves | 1 | 0.1 % |
| materials | 1 | 0.1 % |
| wall | 1 | 0.1 % |
| discretisation | 1 | 0.1 % |
| phase | 1 | 0.1 % |
| jets | 1 | 0.1 % |
| reduce | 1 | 0.1 % |
| ganippa | 1 | 0.1 % |
| rebound | 1 | 0.1 % |
| yoshinobu | 1 | 0.1 % |
| bristles | 1 | 0.1 % |
| plate | 1 | 0.1 % |
| yu. | 1 | 0.1 % |
| fluid | 1 | 0.1 % |
| multiphase | 1 | 0.1 % |
| cause | 1 | 0.1 % |
| oriented | 1 | 0.1 % |
| navier-stokes | 1 | 0.1 % |
| schemes | 1 | 0.1 % |
| two-dimensional | 1 | 0.1 % |
| eeg | 1 | 0.1 % |
| development | 1 | 0.1 % |
| reacting | 1 | 0.1 % |
| mechanism | 1 | 0.1 % |
| shedding | 1 | 0.1 % |
| problem | 1 | 0.1 % |
| hierarchical | 1 | 0.1 % |
| moving | 1 | 0.1 % |
| explain | 1 | 0.1 % |
| dynamics | 1 | 0.1 % |
| control | 1 | 0.1 % |
| computations | 1 | 0.1 % |
| grid | 1 | 0.1 % |
| heat | 1 | 0.1 % |
| product | 1 | 0.1 % |
| 5 | 1 | 0.1 % |
| destruction | 1 | 0.1 % |
| rate | 1 | 0.1 % |
| inner | 1 | 0.1 % |
| study | 1 | 0.1 % |
| perspectives | 1 | 0.1 % |
| determination | 1 | 0.1 % |
| behaviour | 1 | 0.1 % |
| enthalpy | 1 | 0.1 % |
| scheme | 1 | 0.1 % |
| laser-induced | 1 | 0.1 % |
| description | 1 | 0.1 % |
| subgrid-scale | 1 | 0.1 % |
| propellers | 1 | 0.1 % |
| number | 1 | 0.1 % |
| shock | 1 | 0.1 % |
| tsujimoto | 1 | 0.1 % |
| 1894 | 1 | 0.1 % |
| sleipnir_3_w | 1 | 0.1 % |
| journal | 1 | 0.1 % |
| animation | 1 | 0.1 % |
| japikse | 1 | 0.1 % |
| m. | 1 | 0.1 % |
| sydney | 1 | 0.1 % |
| using | 1 | 0.1 % |
| observation | 1 | 0.1 % |
| laser | 1 | 0.1 % |
| near-wall | 1 | 0.1 % |
| bubbles | 1 | 0.1 % |
| test | 1 | 0.1 % |
| express | 1 | 0.1 % |
| critical | 1 | 0.1 % |
| cloud | 1 | 0.1 % |
| r.e. | 1 | 0.1 % |
| mass | 1 | 0.1 % |
| hardware | 1 | 0.1 % |
| dimension | 1 | 0.1 % |
| evaluation | 1 | 0.1 % |
| models | 1 | 0.1 % |
| matsumoto | 1 | 0.1 % |
| how | 1 | 0.1 % |
| hyundai | 1 | 0.1 % |
| chimera | 1 | 0.1 % |
| parameter | 1 | 0.1 % |
| throat | 1 | 0.1 % |
| pumps | 1 | 0.1 % |
| collapsing | 1 | 0.1 % |
| yoshizawa | 1 | 0.1 % |
| inefficiencies | 1 | 0.1 % |
| use | 1 | 0.1 % |
| bodies | 1 | 0.1 % |
| compounds | 1 | 0.1 % |
| behavior | 1 | 0.1 % |
| microprogram | 1 | 0.1 % |
| isenthalpic | 1 | 0.1 % |
| normal | 1 | 0.1 % |
| y | 1 | 0.1 % |
| diverging | 1 | 0.1 % |
| liquid | 1 | 0.1 % |
| williams | 1 | 0.1 % |
| diesel | 1 | 0.1 % |
| dynamic | 1 | 0.1 % |
| distribution | 1 | 0.1 % |
| lertnuwat | 1 | 0.1 % |
| circuit | 1 | 0.1 % |
| vibrations | 1 | 0.1 % |
| cal. | 1 | 0.1 % |
| savchenko | 1 | 0.1 % |
| technique | 1 | 0.1 % |
| equation | 1 | 0.1 % |
| english | 1 | 0.1 % |
| mead | 1 | 0.1 % |
| forces | 1 | 0.1 % |
| oxidize | 1 | 0.1 % |
| cascad | 1 | 0.1 % |
| modelling | 1 | 0.1 % |
| supercavitation—problems | 1 | 0.1 % |
| concepts | 1 | 0.1 % |
| latent | 1 | 0.1 % |
| mixed | 1 | 0.1 % |
| fredgolm | 1 | 0.1 % |
| rans/bem | 1 | 0.1 % |
| asus | 1 | 0.1 % |
| helium | 1 | 0.1 % |
| bubbly | 1 | 0.1 % |
| g134 | 1 | 0.1 % |
| hydrofoils | 1 | 0.1 % |
| valve | 1 | 0.1 % |
| d. | 1 | 0.1 % |
| curve | 1 | 0.1 % |
| s | 1 | 0.1 % |
| ultrasonic | 1 | 0.1 % |
| changes | 1 | 0.1 % |
| ventilation | 1 | 0.1 % |
| pgm-10kc | 1 | 0.1 % |
| impact | 1 | 0.1 % |
| filetype | 1 | 0.1 % |
| topology | 1 | 0.1 % |
| asme | 1 | 0.1 % |
| compressors | 1 | 0.1 % |
| niam | 1 | 0.1 % |
| baghdassarian | 1 | 0.1 % |
| 40/20/40 | 1 | 0.1 % |
| low | 1 | 0.1 % |
| betac | 1 | 0.1 % |
| kuggogkgfd | 1 | 0.1 % |
| g.s. | 1 | 0.1 % |
| surface-piercing | 1 | 0.1 % |
| two- | 1 | 0.1 % |
| rarefaction | 1 | 0.1 % |
| kinematic | 1 | 0.1 % |
| table | 1 | 0.1 % |
| projects | 1 | 0.1 % |
| configuration | 1 | 0.1 % |
| kuiper | 1 | 0.1 % |
| digital | 1 | 0.1 % |
| aging | 1 | 0.1 % |
| linear | 1 | 0.1 % |
| added | 1 | 0.1 % |
| bearing | 1 | 0.1 % |
| from | 1 | 0.1 % |
| real | 1 | 0.1 % |
| disadvantage | 1 | 0.1 % |
| simplified | 1 | 0.1 % |
| kjeldsen | 1 | 0.1 % |
| sprauting | 1 | 0.1 % |
| propulsion- | 1 | 0.1 % |
| large | 1 | 0.1 % |
| lithotripsy | 1 | 0.1 % |
| berntsen | 1 | 0.1 % |
| wigner-ville | 1 | 0.1 % |
| non | 1 | 0.1 % |
| david | 1 | 0.1 % |
| an | 1 | 0.1 % |
| investigations | 1 | 0.1 % |
| conway | 1 | 0.1 % |
| dissipation | 1 | 0.1 % |
| p5n-mn | 1 | 0.1 % |
| frequency | 1 | 0.1 % |
| arndt | 1 | 0.1 % |
| organic | 1 | 0.1 % |
| rudder | 1 | 0.1 % |
| graphic | 1 | 0.1 % |
| process | 1 | 0.1 % |
| near | 1 | 0.1 % |
| calculation | 1 | 0.1 % |
| reynolds | 1 | 0.1 % |
| turbomachinery | 1 | 0.1 % |
| issues | 1 | 0.1 % |
| r | 1 | 0.1 % |
| research | 1 | 0.1 % |
| fortes-patella | 1 | 0.1 % |
| decrease | 1 | 0.1 % |
| greatest | 1 | 0.1 % |
| . | 1 | 0.1 % |
| inside | 1 | 0.1 % |
| studies | 1 | 0.1 % |
| tabbert | 1 | 0.1 % |
| book | 1 | 0.1 % |
| air | 1 | 0.1 % |
| sonoluminescence | 1 | 0.1 % |
| noise | 1 | 0.1 % |
|