| 142 different keywords | Search | Percent |
|---|
| cavitation | 21 | 7.2 % |
| vortex | 11 | 3.7 % |
| of | 10 | 3.4 % |
| on | 7 | 2.4 % |
| pump | 7 | 2.4 % |
| suction | 6 | 2 % |
| water | 5 | 1.7 % |
| for | 5 | 1.7 % |
| orifice | 5 | 1.7 % |
| finite | 4 | 1.3 % |
| jet | 4 | 1.3 % |
| numerical | 4 | 1.3 % |
| and | 4 | 1.3 % |
| erosion | 4 | 1.3 % |
| vlsi | 4 | 1.3 % |
| design | 4 | 1.3 % |
| volume | 4 | 1.3 % |
| re-entrant | 3 | 1 % |
| propeller | 3 | 1 % |
| modelling | 3 | 1 % |
| sheet | 3 | 1 % |
| laser | 3 | 1 % |
| the | 3 | 1 % |
| restriction | 3 | 1 % |
| performance | 3 | 1 % |
| /resolver. | 2 | 0.6 % |
| 2001 | 2 | 0.6 % |
| tipvortex | 2 | 0.6 % |
| area | 2 | 0.6 % |
| time | 2 | 0.6 % |
| cutting | 2 | 0.6 % |
| - | 2 | 0.6 % |
| developments | 2 | 0.6 % |
| law | 2 | 0.6 % |
| bellmouth | 2 | 0.6 % |
| supercavitation | 2 | 0.6 % |
| systems | 2 | 0.6 % |
| hydrofoils | 2 | 0.6 % |
| constitutive | 2 | 0.6 % |
| plates | 2 | 0.6 % |
| two-dimensional | 2 | 0.6 % |
| blade | 2 | 0.6 % |
| [3] g.kuiper/main | 2 | 0.6 % |
| caltechconf. | 2 | 0.6 % |
| simulation | 2 | 0.6 % |
| propellers”. | 2 | 0.6 % |
| -abrasive | 2 | 0.6 % |
| around | 2 | 0.6 % |
| content | 2 | 0.6 % |
| tip | 2 | 0.6 % |
| partially | 2 | 0.6 % |
| digital | 2 | 0.6 % |
| ships | 2 | 0.6 % |
| colloquium | 2 | 0.6 % |
| intake | 2 | 0.6 % |
| caltech. | 2 | 0.6 % |
| netherlannds.-“new | 2 | 0.6 % |
| bubble | 2 | 0.6 % |
| edu/cav2001 | 2 | 0.6 % |
| supercavitating | 2 | 0.6 % |
| lectures | 2 | 0.6 % |
| calculation | 2 | 0.6 % |
| turbomachinery | 2 | 0.6 % |
| pumps | 2 | 0.6 % |
| cavitating | 2 | 0.6 % |
| library.caltech.edu | 2 | 0.6 % |
| inducer | 1 | 0.3 % |
| flow | 1 | 0.3 % |
| pvdf | 1 | 0.3 % |
| sump | 1 | 0.3 % |
| soyama | 1 | 0.3 % |
| clearance | 1 | 0.3 % |
| turbopump | 1 | 0.3 % |
| scaling | 1 | 0.3 % |
| system | 1 | 0.3 % |
| strength | 1 | 0.3 % |
| pipes | 1 | 0.3 % |
| flows | 1 | 0.3 % |
| oscillating | 1 | 0.3 % |
| modeling | 1 | 0.3 % |
| a | 1 | 0.3 % |
| chord | 1 | 0.3 % |
| ho | 1 | 0.3 % |
| plate | 1 | 0.3 % |
| in | 1 | 0.3 % |
| multiphase | 1 | 0.3 % |
| mfnfbgrgeve | 1 | 0.3 % |
| turbine | 1 | 0.3 % |
| corrosion | 1 | 0.3 % |
| ” | 1 | 0.3 % |
| fluent | 1 | 0.3 % |
| position | 1 | 0.3 % |
| partial | 1 | 0.3 % |
| mecanism | 1 | 0.3 % |
| formulas | 1 | 0.3 % |
| inlet | 1 | 0.3 % |
| drag | 1 | 0.3 % |
| hydrofoil | 1 | 0.3 % |
| 2d | 1 | 0.3 % |
| study | 1 | 0.3 % |
| based | 1 | 0.3 % |
| problems | 1 | 0.3 % |
| self-timed | 1 | 0.3 % |
| applications | 1 | 0.3 % |
| observations | 1 | 0.3 % |
| propellers | 1 | 0.3 % |
| some | 1 | 0.3 % |
| with | 1 | 0.3 % |
| number | 1 | 0.3 % |
| added | 1 | 0.3 % |
| codes | 1 | 0.3 % |
| into | 1 | 0.3 % |
| advantages | 1 | 0.3 % |
| body | 1 | 0.3 % |
| mosflipflop | 1 | 0.3 % |
| causes | 1 | 0.3 % |
| thickness | 1 | 0.3 % |
| given | 1 | 0.3 % |
| investigations | 1 | 0.3 % |
| or | 1 | 0.3 % |
| mass | 1 | 0.3 % |
| hierarchy | 1 | 0.3 % |
| models | 1 | 0.3 % |
| gdfdfdfwshkwjkqwujgfgfgft | 1 | 0.3 % |
| v | 1 | 0.3 % |
| leading | 1 | 0.3 % |
| flat | 1 | 0.3 % |
| compressible | 1 | 0.3 % |
| r | 1 | 0.3 % |
| at | 1 | 0.3 % |
| inside | 1 | 0.3 % |
| experimental | 1 | 0.3 % |
| edge | 1 | 0.3 % |
| approximation | 1 | 0.3 % |
| cavities | 1 | 0.3 % |
| centrifugal | 1 | 0.3 % |
| resses | 1 | 0.3 % |
| effects | 1 | 0.3 % |
| unsteady | 1 | 0.3 % |
| capacity | 1 | 0.3 % |
| prediction | 1 | 0.3 % |
| slender | 1 | 0.3 % |
|