| 412 different keywords | Search | Percent |
|---|
| cavitation | 68 | 6.8 % |
| of | 47 | 4.7 % |
| in | 32 | 3.2 % |
| and | 29 | 2.9 % |
| a | 22 | 2.2 % |
| the | 15 | 1.5 % |
| on | 13 | 1.3 % |
| bubble | 12 | 1.2 % |
| flow | 11 | 1.1 % |
| vortex | 11 | 1.1 % |
| supercavitation | 8 | 0.8 % |
| http | 8 | 0.8 % |
| orifice | 8 | 0.8 % |
| propeller | 8 | 0.8 % |
| cavitating | 8 | 0.8 % |
| numerical | 7 | 0.7 % |
| storage | 7 | 0.7 % |
| pump | 7 | 0.7 % |
| unsteady | 7 | 0.7 % |
| lisp | 7 | 0.7 % |
| for | 7 | 0.7 % |
| management | 7 | 0.7 % |
| experimental | 7 | 0.7 % |
| scale | 6 | 0.6 % |
| collapse | 6 | 0.6 % |
| ventilated | 6 | 0.6 % |
| with | 6 | 0.6 % |
| supercavitating | 6 | 0.6 % |
| counterjet | 5 | 0.5 % |
| rebound | 5 | 0.5 % |
| simulation | 5 | 0.5 % |
| vlsi | 5 | 0.5 % |
| instability | 5 | 0.5 % |
| mass | 5 | 0.5 % |
| acoustic | 5 | 0.5 % |
| partial | 5 | 0.5 % |
| tip | 5 | 0.5 % |
| added | 5 | 0.5 % |
| to | 5 | 0.5 % |
| noise | 5 | 0.5 % |
| inducer | 4 | 0.4 % |
| used | 4 | 0.4 % |
| study | 4 | 0.4 % |
| laser-induced | 4 | 0.4 % |
| design | 4 | 0.4 % |
| tunnel | 4 | 0.4 % |
| laser | 4 | 0.4 % |
| kucherenko | 4 | 0.4 % |
| how | 4 | 0.4 % |
| cavities | 4 | 0.4 % |
| emission | 4 | 0.4 % |
| behavior | 4 | 0.4 % |
| restriction | 4 | 0.4 % |
| pressure | 4 | 0.4 % |
| & | 4 | 0.4 % |
| shamko | 4 | 0.4 % |
| analysis | 4 | 0.4 % |
| flows | 4 | 0.4 % |
| investigation | 4 | 0.4 % |
| coefficient | 4 | 0.4 % |
| developed | 4 | 0.4 % |
| effect | 4 | 0.4 % |
| turbomachinery | 4 | 0.4 % |
| h | 4 | 0.4 % |
| centrifugal | 4 | 0.4 % |
| jets | 3 | 0.3 % |
| solid | 3 | 0.3 % |
| number | 3 | 0.3 % |
| cavity | 3 | 0.3 % |
| characteristics | 3 | 0.3 % |
| observation | 3 | 0.3 % |
| simulations | 3 | 0.3 % |
| blades | 3 | 0.3 % |
| 2001 | 3 | 0.3 % |
| hydrofoil | 3 | 0.3 % |
| supercavity | 3 | 0.3 % |
| theoreticalanalysisofunsteadybladeloadingofinducersunderrotatingcavitation-caltechconf | 3 | 0.3 % |
| calculation | 3 | 0.3 % |
| inception | 3 | 0.3 % |
| types | 3 | 0.3 % |
| effects | 3 | 0.3 % |
| boundaries | 2 | 0.2 % |
| system | 2 | 0.2 % |
| time | 2 | 0.2 % |
| anewparametertopredictcavitationerosion-caltechconf | 2 | 0.2 % |
| nand | 2 | 0.2 % |
| experiment | 2 | 0.2 % |
| model | 2 | 0.2 % |
| fluid | 2 | 0.2 % |
| 1999 | 2 | 0.2 % |
| type | 2 | 0.2 % |
| mechanism | 2 | 0.2 % |
| damaged | 2 | 0.2 % |
| erosive | 2 | 0.2 % |
| similaritiesandgeometricaleffectsonrotatingcavitationintwoscaltedcentrifugalpumps-caltechconf | 2 | 0.2 % |
| backflow | 2 | 0.2 % |
| piping | 2 | 0.2 % |
| affect | 2 | 0.2 % |
| density | 2 | 0.2 % |
| size | 2 | 0.2 % |
| asymptotic | 2 | 0.2 % |
| cavitationerosionmechanism | 2 | 0.2 % |
| approach | 2 | 0.2 % |
| bubbles | 2 | 0.2 % |
| algorithm | 2 | 0.2 % |
| compressibility | 2 | 0.2 % |
| axial | 2 | 0.2 % |
| pumps | 2 | 0.2 % |
| jp | 2 | 0.2 % |
| rules | 2 | 0.2 % |
| curved | 2 | 0.2 % |
| hofmann | 2 | 0.2 % |
| ariane5 | 2 | 0.2 % |
| //caltechconf.library.caltech.edu/143/1/pope.pdf | 2 | 0.2 % |
| lohrberg | 2 | 0.2 % |
| jet | 2 | 0.2 % |
| properties | 2 | 0.2 % |
| rectangular | 2 | 0.2 % |
| introduction | 2 | 0.2 % |
| is | 2 | 0.2 % |
| limits | 2 | 0.2 % |
| have | 2 | 0.2 % |
| erosion | 2 | 0.2 % |
| structures | 2 | 0.2 % |
| tploxinducerdesignstrategiestoenhancecavitatingperformance-caltechconf | 2 | 0.2 % |
| turbine | 2 | 0.2 % |
| induced | 2 | 0.2 % |
| full | 2 | 0.2 % |
| fluent | 2 | 0.2 % |
| instabilities | 2 | 0.2 % |
| low | 2 | 0.2 % |
| orifices | 2 | 0.2 % |
| 2d | 2 | 0.2 % |
| surge | 2 | 0.2 % |
| franc | 2 | 0.2 % |
| simple | 2 | 0.2 % |
| vehicle | 2 | 0.2 % |
| measurements | 2 | 0.2 % |
| radiated | 2 | 0.2 % |
| numericalsumulationsoftheinteractionbetweenpressurewavesandsolidboundaries-caltechconf | 2 | 0.2 % |
| an | 2 | 0.2 % |
| investigations | 2 | 0.2 % |
| does | 2 | 0.2 % |
| rudder | 2 | 0.2 % |
| kaplan | 2 | 0.2 % |
| near | 2 | 0.2 % |
| interaction | 2 | 0.2 % |
| studies | 2 | 0.2 % |
| structure | 2 | 0.2 % |
| you | 1 | 0.1 % |
| 90 | 1 | 0.1 % |
| ieee | 1 | 0.1 % |
| towardsmorerealisticmodelsofcomputationforvlsi-caltechconf | 1 | 0.1 % |
| conical | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/66/1/savchenko.pdf | 1 | 0.1 % |
| reasonably | 1 | 0.1 % |
| finite | 1 | 0.1 % |
| power | 1 | 0.1 % |
| npsh | 1 | 0.1 % |
| pumping? | 1 | 0.1 % |
| serebryakov | 1 | 0.1 % |
| shapes | 1 | 0.1 % |
| inducer. | 1 | 0.1 % |
| waves | 1 | 0.1 % |
| important | 1 | 0.1 % |
| reduction | 1 | 0.1 % |
| underwater | 1 | 0.1 % |
| thisworkwassponsoredbythedepartmentoftheairforce. | 1 | 0.1 % |
| rule | 1 | 0.1 % |
| still | 1 | 0.1 % |
| disadvantages | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/85/0/cav2001_sessionb9.001.html | 1 | 0.1 % |
| programming | 1 | 0.1 % |
| generations | 1 | 0.1 % |
| speed | 1 | 0.1 % |
| 2000 | 1 | 0.1 % |
| variation | 1 | 0.1 % |
| can | 1 | 0.1 % |
| carolyn | 1 | 0.1 % |
| turbopumps | 1 | 0.1 % |
| stability | 1 | 0.1 % |
| pla | 1 | 0.1 % |
| experimentalanalysisand2dnumericalsimulationofunsteadyflowinbladecascade-caltechconf | 1 | 0.1 % |
| network | 1 | 0.1 % |
| plate | 1 | 0.1 % |
| acomputerstudyofelectron-electroninteractioninhighdensityelectronbeams-caltechconf | 1 | 0.1 % |
| pdf | 1 | 0.1 % |
| two-dimensional | 1 | 0.1 % |
| data | 1 | 0.1 % |
| axisymmetrical | 1 | 0.1 % |
| watson | 1 | 0.1 % |
| by | 1 | 0.1 % |
| correlation | 1 | 0.1 % |
| chip | 1 | 0.1 % |
| computational | 1 | 0.1 % |
| gates | 1 | 0.1 % |
| 2-d | 1 | 0.1 % |
| forrestructurablevlsi | 1 | 0.1 % |
| vibration | 1 | 0.1 % |
| shedding | 1 | 0.1 % |
| restrepo | 1 | 0.1 % |
| coutier-delgosha | 1 | 0.1 % |
| mechanics | 1 | 0.1 % |
| moving | 1 | 0.1 % |
| knapp | 1 | 0.1 % |
| dynamics | 1 | 0.1 % |
| langragian | 1 | 0.1 % |
| global | 1 | 0.1 % |
| runners | 1 | 0.1 % |
| water | 1 | 0.1 % |
| why | 1 | 0.1 % |
| international | 1 | 0.1 % |
| ultrasound | 1 | 0.1 % |
| rate | 1 | 0.1 % |
| mpcs | 1 | 0.1 % |
| drag | 1 | 0.1 % |
| somemodelsofpredictionofsupercavitationflowsbasedonslenderbodyapproximation-caltechconf | 1 | 0.1 % |
| cavitationtunneltestsforpropellernoiseofafrvandcomparisonswithfull-scalemeasurements-caltechconf | 1 | 0.1 % |
| determination | 1 | 0.1 % |
| problems | 1 | 0.1 % |
| weber | 1 | 0.1 % |
| tyes | 1 | 0.1 % |
| behaviour | 1 | 0.1 % |
| processor | 1 | 0.1 % |
| second | 1 | 0.1 % |
| applications | 1 | 0.1 % |
| difference | 1 | 0.1 % |
| behind | 1 | 0.1 % |
| tj. | 1 | 0.1 % |
| empirical | 1 | 0.1 % |
| symposium | 1 | 0.1 % |
| physics | 1 | 0.1 % |
| body | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/128/1/jetoxcav2001.pdf | 1 | 0.1 % |
| sections | 1 | 0.1 % |
| cabitation | 1 | 0.1 % |
| influence | 1 | 0.1 % |
| create | 1 | 0.1 % |
| judge | 1 | 0.1 % |
| japikse | 1 | 0.1 % |
| numerical/experimental | 1 | 0.1 % |
| thickness | 1 | 0.1 % |
| ittc | 1 | 0.1 % |
| surface | 1 | 0.1 % |
| population | 1 | 0.1 % |
| pipe | 1 | 0.1 % |
| j | 1 | 0.1 % |
| methods | 1 | 0.1 % |
| 100 | 1 | 0.1 % |
| balance | 1 | 0.1 % |
| liquids | 1 | 0.1 % |
| associated | 1 | 0.1 % |
| direct | 1 | 0.1 % |
| pipe? | 1 | 0.1 % |
| cl | 1 | 0.1 % |
| complexity | 1 | 0.1 % |
| ibm | 1 | 0.1 % |
| welcometocaltechconf-caltechconf | 1 | 0.1 % |
| sheet/cloud | 1 | 0.1 % |
| coating | 1 | 0.1 % |
| 1973 | 1 | 0.1 % |
| use | 1 | 0.1 % |
| vof | 1 | 0.1 % |
| fourth | 1 | 0.1 % |
| approximation | 1 | 0.1 % |
| asynchronous | 1 | 0.1 % |
| sato | 1 | 0.1 % |
| tests | 1 | 0.1 % |
| nose | 1 | 0.1 % |
| prediction | 1 | 0.1 % |
| gradients | 1 | 0.1 % |
| performance | 1 | 0.1 % |
| compare | 1 | 0.1 % |
| eulerian | 1 | 0.1 % |
| which | 1 | 0.1 % |
| pipelines | 1 | 0.1 % |
| thermal | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/42/1/pasadena.ps | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/70/1/cav2001_b5006.pdf | 1 | 0.1 % |
| examples | 1 | 0.1 % |
| errosion | 1 | 0.1 % |
| damping | 1 | 0.1 % |
| inverse | 1 | 0.1 % |
| 000 | 1 | 0.1 % |
| distribution | 1 | 0.1 % |
| nonlinear | 1 | 0.1 % |
| takashi | 1 | 0.1 % |
| roll-up | 1 | 0.1 % |
| circuit | 1 | 0.1 % |
| vlsiandtechnologicalinnovation-caltechconf | 1 | 0.1 % |
| laser-produced | 1 | 0.1 % |
| but | 1 | 0.1 % |
| small | 1 | 0.1 % |
| savchenko | 1 | 0.1 % |
| over | 1 | 0.1 % |
| spectral | 1 | 0.1 % |
| patella | 1 | 0.1 % |
| 5. how | 1 | 0.1 % |
| it | 1 | 0.1 % |
| sonic | 1 | 0.1 % |
| modelling | 1 | 0.1 % |
| 2d-curved | 1 | 0.1 % |
| sessiona5.001 | 1 | 0.1 % |
| index | 1 | 0.1 % |
| tunel | 1 | 0.1 % |
| butterfly | 1 | 0.1 % |
| cavitator | 1 | 0.1 % |
| breakup | 1 | 0.1 % |
| thrust | 1 | 0.1 % |
| a. | 1 | 0.1 % |
| countermeasure | 1 | 0.1 % |
| soft | 1 | 0.1 % |
| full-scale | 1 | 0.1 % |
| valve | 1 | 0.1 % |
| c | 1 | 0.1 % |
| hvg | 1 | 0.1 % |
| pins | 1 | 0.1 % |
| cav | 1 | 0.1 % |
| ric | 1 | 0.1 % |
| thick | 1 | 0.1 % |
| hydrodynamic | 1 | 0.1 % |
| lauterborn | 1 | 0.1 % |
| filetype | 1 | 0.1 % |
| v.v. | 1 | 0.1 % |
| axially | 1 | 0.1 % |
| suction | 1 | 0.1 % |
| available | 1 | 0.1 % |
| overviewofindustrialandrocketturbopumpinducerdesign-caltechconf | 1 | 0.1 % |
| transistor | 1 | 0.1 % |
| mean | 1 | 0.1 % |
| through | 1 | 0.1 % |
| theoretical | 1 | 0.1 % |
| marotin | 1 | 0.1 % |
| systolic | 1 | 0.1 % |
| recent | 1 | 0.1 % |
| turbines | 1 | 0.1 % |
| cavitatinginducerinstabilities | 1 | 0.1 % |
| condition | 1 | 0.1 % |
| foil | 1 | 0.1 % |
| kinematic | 1 | 0.1 % |
| rise | 1 | 0.1 % |
| micro | 1 | 0.1 % |
| layout | 1 | 0.1 % |
| hydraulic | 1 | 0.1 % |
| keiichi | 1 | 0.1 % |
| spectrum | 1 | 0.1 % |
| symmetric | 1 | 0.1 % |
| comparisons | 1 | 0.1 % |
| digital | 1 | 0.1 % |
| overlapping | 1 | 0.1 % |
| secondary | 1 | 0.1 % |
| 20-23 | 1 | 0.1 % |
| wiki | 1 | 0.1 % |
| logic | 1 | 0.1 % |
| linear | 1 | 0.1 % |
| tokumasu | 1 | 0.1 % |
| do | 1 | 0.1 % |
| delay | 1 | 0.1 % |
| channel | 1 | 0.1 % |
| find | 1 | 0.1 % |
| advantages | 1 | 0.1 % |
| velocity | 1 | 0.1 % |
| from | 1 | 0.1 % |
| joint | 1 | 0.1 % |
| propagation | 1 | 0.1 % |
| method | 1 | 0.1 % |
| frv | 1 | 0.1 % |
| device | 1 | 0.1 % |
| optical | 1 | 0.1 % |
| supercavitate | 1 | 0.1 % |
| functionalverificationinaninteractivesymbolicicdesignenvironment-caltechconf | 1 | 0.1 % |
| nozzle | 1 | 0.1 % |
| wake | 1 | 0.1 % |
| nominal | 1 | 0.1 % |
| david | 1 | 0.1 % |
| priority | 1 | 0.1 % |
| //caltechconf.library.caltech.edu/187/ | 1 | 0.1 % |
| merkle | 1 | 0.1 % |
| acceleration | 1 | 0.1 % |
| impellor | 1 | 0.1 % |
| numericalmodelingofsheetandtipvortexcavitationwithfluent5-caltechconf | 1 | 0.1 % |
| boundary | 1 | 0.1 % |
| field | 1 | 0.1 % |
| numerical/experimental | 1 | 0.1 % |
| high-speed | 1 | 0.1 % |
| fortes | 1 | 0.1 % |
| theory | 1 | 0.1 % |
| 1998 | 1 | 0.1 % |
| melville | 1 | 0.1 % |
| shape | 1 | 0.1 % |
| issues | 1 | 0.1 % |
| compressible | 1 | 0.1 % |
| degree | 1 | 0.1 % |
| vehicles | 1 | 0.1 % |
| solutions | 1 | 0.1 % |
| predictionofthe2-dunsteadysupercavityshapes-caltechconf | 1 | 0.1 % |
| high | 1 | 0.1 % |
| current | 1 | 0.1 % |
| . | 1 | 0.1 % |
| twodimensional | 1 | 0.1 % |
| cav2001 | 1 | 0.1 % |
| expansion | 1 | 0.1 % |
| between | 1 | 0.1 % |
| application | 1 | 0.1 % |
| 1955 | 1 | 0.1 % |
| leakage | 1 | 0.1 % |
| june | 1 | 0.1 % |
| measure | 1 | 0.1 % |
| slender | 1 | 0.1 % |
| ideal | 1 | 0.1 % |
| air | 1 | 0.1 % |
| piercing | 1 | 0.1 % |