| 939 different keywords | Search | Percent |
|---|
| cavitation | 253 | 7.6 % |
| of | 139 | 4.1 % |
| orifice | 106 | 3.1 % |
| in | 62 | 1.8 % |
| restriction | 59 | 1.7 % |
| a | 43 | 1.2 % |
| and | 42 | 1.2 % |
| flow | 40 | 1.2 % |
| pdf | 37 | 1.1 % |
| propeller | 37 | 1.1 % |
| pump | 32 | 0.9 % |
| on | 31 | 0.9 % |
| bubble | 31 | 0.9 % |
| for | 29 | 0.8 % |
| vortex | 29 | 0.8 % |
| cavitating | 27 | 0.8 % |
| design | 25 | 0.7 % |
| the | 22 | 0.6 % |
| experimental | 22 | 0.6 % |
| numerical | 21 | 0.6 % |
| flows | 20 | 0.6 % |
| plate | 20 | 0.6 % |
| noise | 20 | 0.6 % |
| model | 18 | 0.5 % |
| supercavitation | 18 | 0.5 % |
| water | 18 | 0.5 % |
| simulation | 17 | 0.5 % |
| test | 16 | 0.4 % |
| fluent | 16 | 0.4 % |
| number | 14 | 0.4 % |
| filetype | 14 | 0.4 % |
| tunnel | 14 | 0.4 % |
| centrifugal | 14 | 0.4 % |
| unsteady | 13 | 0.3 % |
| to | 13 | 0.3 % |
| turbopump | 12 | 0.3 % |
| experiment | 12 | 0.3 % |
| pressure | 12 | 0.3 % |
| supercavitating | 12 | 0.3 % |
| types | 12 | 0.3 % |
| cavity | 12 | 0.3 % |
| nexearch | 12 | 0.3 % |
| study | 11 | 0.3 % |
| symposium | 11 | 0.3 % |
| tip | 11 | 0.3 % |
| with | 11 | 0.3 % |
| inducer | 11 | 0.3 % |
| effect | 11 | 0.3 % |
| nozzle | 11 | 0.3 % |
| 2001 | 10 | 0.3 % |
| analysis | 10 | 0.3 % |
| butterfly | 10 | 0.3 % |
| naca | 10 | 0.3 % |
| shock | 10 | 0.3 % |
| rudder | 10 | 0.3 % |
| phase | 9 | 0.2 % |
| instability | 9 | 0.2 % |
| erosion | 9 | 0.2 % |
| paper | 9 | 0.2 % |
| turbine | 9 | 0.2 % |
| hydrofoil | 9 | 0.2 % |
| cav2001 | 9 | 0.2 % |
| international | 9 | 0.2 % |
| wave | 9 | 0.2 % |
| ship | 9 | 0.2 % |
| valve | 9 | 0.2 % |
| kaplan | 9 | 0.2 % |
| submerged | 9 | 0.2 % |
| velocity | 8 | 0.2 % |
| sae | 8 | 0.2 % |
| rocket | 8 | 0.2 % |
| 0015 | 8 | 0.2 % |
| propellers | 8 | 0.2 % |
| approach | 8 | 0.2 % |
| pumps | 8 | 0.2 % |
| partial | 8 | 0.2 % |
| effects | 8 | 0.2 % |
| dynamics | 7 | 0.2 % |
| surface | 7 | 0.2 % |
| coefficient | 7 | 0.2 % |
| an | 7 | 0.2 % |
| boundary | 7 | 0.2 % |
| kinnas | 7 | 0.2 % |
| lagrangian | 7 | 0.2 % |
| impeller | 7 | 0.2 % |
| tab_hty | 7 | 0.2 % |
| using | 7 | 0.2 % |
| equation | 7 | 0.2 % |
| cfd | 7 | 0.2 % |
| at | 7 | 0.2 % |
| underwater | 6 | 0.1 % |
| t. | 6 | 0.1 % |
| lindau | 6 | 0.1 % |
| fluid | 6 | 0.1 % |
| observation | 6 | 0.1 % |
| pipe | 6 | 0.1 % |
| how | 6 | 0.1 % |
| oscillation | 6 | 0.1 % |
| liquid | 6 | 0.1 % |
| jet | 6 | 0.1 % |
| quality | 6 | 0.1 % |
| ventilated | 6 | 0.1 % |
| sizing | 6 | 0.1 % |
| arndt | 6 | 0.1 % |
| turbulent | 6 | 0.1 % |
| dynamic | 6 | 0.1 % |
| investigation | 6 | 0.1 % |
| sheet | 6 | 0.1 % |
| helium | 6 | 0.1 % |
| cav | 6 | 0.1 % |
| orifices | 6 | 0.1 % |
| diameter | 6 | 0.1 % |
| energy | 5 | 0.1 % |
| attached | 5 | 0.1 % |
| protection | 5 | 0.1 % |
| numerical/experimental | 5 | 0.1 % |
| behavior | 5 | 0.1 % |
| template | 5 | 0.1 % |
| hydrodynamic | 5 | 0.1 % |
| through | 5 | 0.1 % |
| wake | 5 | 0.1 % |
| maxey | 5 | 0.1 % |
| speed | 5 | 0.1 % |
| cryogenic | 5 | 0.1 % |
| et | 5 | 0.1 % |
| tests | 5 | 0.1 % |
| turbo | 5 | 0.1 % |
| bubbly | 5 | 0.1 % |
| suction | 5 | 0.1 % |
| method | 5 | 0.1 % |
| high | 5 | 0.1 % |
| marine | 4 | 0.1 % |
| intraluminal | 4 | 0.1 % |
| spilled | 4 | 0.1 % |
| kavitation | 4 | 0.1 % |
| journal | 4 | 0.1 % |
| j | 4 | 0.1 % |
| scale | 4 | 0.1 % |
| killing | 4 | 0.1 % |
| hull | 4 | 0.1 % |
| is | 4 | 0.1 % |
| hydrodynamics | 4 | 0.1 % |
| length | 4 | 0.1 % |
| acoustic | 4 | 0.1 % |
| ventilation | 4 | 0.1 % |
| rotating | 4 | 0.1 % |
| blade | 4 | 0.1 % |
| restricting | 4 | 0.1 % |
| asme | 4 | 0.1 % |
| oil | 4 | 0.1 % |
| utilization | 4 | 0.1 % |
| motion | 4 | 0.1 % |
| engine | 4 | 0.1 % |
| wang | 4 | 0.1 % |
| reboud | 4 | 0.1 % |
| waves | 4 | 0.1 % |
| comparison | 4 | 0.1 % |
| geometry | 4 | 0.1 % |
| vibration | 4 | 0.1 % |
| discharge | 4 | 0.1 % |
| characteristics | 4 | 0.1 % |
| turbomachines | 4 | 0.1 % |
| cavities | 4 | 0.1 % |
| prediction | 4 | 0.1 % |
| – | 4 | 0.1 % |
| two | 4 | 0.1 % |
| dispersing | 4 | 0.1 % |
| modelling | 4 | 0.1 % |
| jules | 4 | 0.1 % |
| s | 4 | 0.1 % |
| keller | 4 | 0.1 % |
| planktons | 4 | 0.1 % |
| frequency | 4 | 0.1 % |
| environmental | 4 | 0.1 % |
| calculation | 4 | 0.1 % |
| abstract | 4 | 0.1 % |
| particle | 3 | 0 % |
| what | 3 | 0 % |
| measurement | 3 | 0 % |
| equilibrium | 3 | 0 % |
| scaling | 3 | 0 % |
| incipient | 3 | 0 % |
| prop | 3 | 0 % |
| hydrogen | 3 | 0 % |
| 1999 | 3 | 0 % |
| farrell | 3 | 0 % |
| rate | 3 | 0 % |
| kevin | 3 | 0 % |
| change | 3 | 0 % |
| density | 3 | 0 % |
| lift | 3 | 0 % |
| lynn | 3 | 0 % |
| nuclei | 3 | 0 % |
| pitch | 3 | 0 % |
| taylor | 3 | 0 % |
| collapse | 3 | 0 % |
| performance | 3 | 0 % |
| technical | 3 | 0 % |
| sound | 3 | 0 % |
| regiane | 3 | 0 % |
| distribution | 3 | 0 % |
| patella | 3 | 0 % |
| restricted | 3 | 0 % |
| hydrofoils | 3 | 0 % |
| full-scale | 3 | 0 % |
| djeridi | 3 | 0 % |
| inducers | 3 | 0 % |
| layer | 3 | 0 % |
| measurements | 3 | 0 % |
| frv | 3 | 0 % |
| japanese | 3 | 0 % |
| hydro | 3 | 0 % |
| investigations | 3 | 0 % |
| fortes | 3 | 0 % |
| s. | 3 | 0 % |
| compressible | 3 | 0 % |
| interaction | 3 | 0 % |
| research | 3 | 0 % |
| fortes-patella | 3 | 0 % |
| between | 3 | 0 % |
| 3d | 3 | 0 % |
| strouhal | 3 | 0 % |
| burgess | 3 | 0 % |
| modeling | 3 | 0 % |
| fully | 3 | 0 % |
| content | 3 | 0 % |
| ultrasound | 3 | 0 % |
| behaviour | 3 | 0 % |
| hole | 3 | 0 % |
| collapsing | 3 | 0 % |
| tot | 3 | 0 % |
| fourth | 3 | 0 % |
| orfice | 3 | 0 % |
| insean | 3 | 0 % |
| three-dimensional | 3 | 0 % |
| vol. | 3 | 0 % |
| induced | 3 | 0 % |
| ultrasonic | 3 | 0 % |
| latest | 3 | 0 % |
| takahira | 3 | 0 % |
| instabilities | 3 | 0 % |
| hydrophone | 3 | 0 % |
| waterjet | 3 | 0 % |
| lattice | 3 | 0 % |
| circular | 3 | 0 % |
| installation | 3 | 0 % |
| from | 3 | 0 % |
| homogeneous | 3 | 0 % |
| r | 3 | 0 % |
| rayleigh | 3 | 0 % |
| l. | 3 | 0 % |
| multi | 3 | 0 % |
| piercing | 3 | 0 % |
| figure | 2 | 0 % |
| wall | 2 | 0 % |
| developments | 2 | 0 % |
| ikohagi | 2 | 0 % |
| super | 2 | 0 % |
| tgrid | 2 | 0 % |
| lab | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| plates | 2 | 0 % |
| re | 2 | 0 % |
| check | 2 | 0 % |
| incompressible | 2 | 0 % |
| avoid | 2 | 0 % |
| vibratory | 2 | 0 % |
| vortices | 2 | 0 % |
| inlet | 2 | 0 % |
| kedrinskii | 2 | 0 % |
| gate | 2 | 0 % |
| drag | 2 | 0 % |
| vapor | 2 | 0 % |
| explosion | 2 | 0 % |
| gopalan | 2 | 0 % |
| piping | 2 | 0 % |
| conditions | 2 | 0 % |
| i. | 2 | 0 % |
| california | 2 | 0 % |
| injector | 2 | 0 % |
| tsujimoto | 2 | 0 % |
| intake | 2 | 0 % |
| pp | 2 | 0 % |
| screen | 2 | 0 % |
| ittc | 2 | 0 % |
| population | 2 | 0 % |
| münchen | 2 | 0 % |
| about | 2 | 0 % |
| reducing | 2 | 0 % |
| ring | 2 | 0 % |
| r. | 2 | 0 % |
| de | 2 | 0 % |
| entrant | 2 | 0 % |
| relation | 2 | 0 % |
| wing | 2 | 0 % |
| convergent-divergent | 2 | 0 % |
| microjet | 2 | 0 % |
| rayleigh–plesset | 2 | 0 % |
| horizontal | 2 | 0 % |
| cone | 2 | 0 % |
| sump | 2 | 0 % |
| related | 2 | 0 % |
| low-specific-speed | 2 | 0 % |
| panel | 2 | 0 % |
| fluids | 2 | 0 % |
| g. | 2 | 0 % |
| hiroyuki | 2 | 0 % |
| astm | 2 | 0 % |
| ceo | 2 | 0 % |
| stokes | 2 | 0 % |
| oti | 2 | 0 % |
| two-phase | 2 | 0 % |
| tu | 2 | 0 % |
| webkr | 2 | 0 % |
| valves | 2 | 0 % |
| aerospace | 2 | 0 % |
| under | 2 | 0 % |
| turbines | 2 | 0 % |
| distance | 2 | 0 % |
| clusters | 2 | 0 % |
| line | 2 | 0 % |
| francesco | 2 | 0 % |
| angle | 2 | 0 % |
| large | 2 | 0 % |
| berntsen | 2 | 0 % |
| converging-diverging | 2 | 0 % |
| or | 2 | 0 % |
| treatment | 2 | 0 % |
| theory | 2 | 0 % |
| reynolds | 2 | 0 % |
| shape | 2 | 0 % |
| damage | 2 | 0 % |
| microbubbles | 2 | 0 % |
| application | 2 | 0 % |
| working | 2 | 0 % |
| vs | 2 | 0 % |
| passage | 2 | 0 % |
| salvatore | 2 | 0 % |
| explosions | 2 | 0 % |
| j. | 2 | 0 % |
| re-entrant | 2 | 0 % |
| sigma | 2 | 0 % |
| 2000 | 2 | 0 % |
| 551-581 | 2 | 0 % |
| les | 2 | 0 % |
| tank | 2 | 0 % |
| multiphase | 2 | 0 % |
| senocak | 2 | 0 % |
| circulation | 2 | 0 % |
| www.cav2001.library.caltech.edu | 2 | 0 % |
| shedding | 2 | 0 % |
| sciences | 2 | 0 % |
| as | 2 | 0 % |
| 37 | 2 | 0 % |
| 5 | 2 | 0 % |
| apparatus | 2 | 0 % |
| element | 2 | 0 % |
| modified | 2 | 0 % |
| body | 2 | 0 % |
| cav01 | 2 | 0 % |
| heister | 2 | 0 % |
| shibata | 2 | 0 % |
| side | 2 | 0 % |
| chen | 2 | 0 % |
| critical | 2 | 0 % |
| eventrates | 2 | 0 % |
| new | 2 | 0 % |
| compressibility | 2 | 0 % |
| en | 2 | 0 % |
| downstream | 2 | 0 % |
| 6 | 2 | 0 % |
| n | 2 | 0 % |
| burrill | 2 | 0 % |
| relative | 2 | 0 % |
| w. | 2 | 0 % |
| conference | 2 | 0 % |
| k. | 2 | 0 % |
| shyy | 2 | 0 % |
| progress | 2 | 0 % |
| mixed | 2 | 0 % |
| d. | 2 | 0 % |
| head | 2 | 0 % |
| stinebring | 2 | 0 % |
| alignment | 2 | 0 % |
| rarefaction | 2 | 0 % |
| testing | 2 | 0 % |
| plesset | 2 | 0 % |
| validation | 2 | 0 % |
| hydraulic | 2 | 0 % |
| btn | 2 | 0 % |
| trans. | 2 | 0 % |
| range | 2 | 0 % |
| ships | 2 | 0 % |
| joint | 2 | 0 % |
| dissertation | 2 | 0 % |
| 66 | 2 | 0 % |
| material | 2 | 0 % |
| lifting | 2 | 0 % |
| mixed-flow | 2 | 0 % |
| high-speed | 2 | 0 % |
| near | 2 | 0 % |
| report | 2 | 0 % |
| 1998 | 2 | 0 % |
| inception | 2 | 0 % |
| v-2 | 2 | 0 % |
| foils | 2 | 0 % |
| al. | 2 | 0 % |
| leakage | 2 | 0 % |
| structure | 2 | 0 % |
| air | 2 | 0 % |
| mpa | 1 | 0 % |
| ki | 1 | 0 % |
| mach | 1 | 0 % |
| closure | 1 | 0 % |
| caviation | 1 | 0 % |
| hose | 1 | 0 % |
| projectile | 1 | 0 % |
| finite | 1 | 0 % |
| life | 1 | 0 % |
| forming | 1 | 0 % |
| constrained | 1 | 0 % |
| portal.acm.org/citation.cfm?id=1360975 | 1 | 0 % |
| competitor | 1 | 0 % |
| materials | 1 | 0 % |
| again | 1 | 0 % |
| nishida | 1 | 0 % |
| threshold | 1 | 0 % |
| system | 1 | 0 % |
| azipod | 1 | 0 % |
| 4th | 1 | 0 % |
| osscialtion | 1 | 0 % |
| bernoulli | 1 | 0 % |
| jets | 1 | 0 % |
| ganippa | 1 | 0 % |
| yoshinobu | 1 | 0 % |
| henrik | 1 | 0 % |
| kt | 1 | 0 % |
| predicting | 1 | 0 % |
| tsien | 1 | 0 % |
| cavitation. | 1 | 0 % |
| coefficients | 1 | 0 % |
| national | 1 | 0 % |
| k | 1 | 0 % |
| cause | 1 | 0 % |
| piere | 1 | 0 % |
| setting | 1 | 0 % |
| al.; | 1 | 0 % |
| by | 1 | 0 % |
| nucleation | 1 | 0 % |
| pp. | 1 | 0 % |
| inch | 1 | 0 % |
| phil. | 1 | 0 % |
| runner | 1 | 0 % |
| project | 1 | 0 % |
| spirale | 1 | 0 % |
| industrial | 1 | 0 % |
| homo | 1 | 0 % |
| caltech | 1 | 0 % |
| stutz | 1 | 0 % |
| structural | 1 | 0 % |
| coalescence | 1 | 0 % |
| grid | 1 | 0 % |
| requirements | 1 | 0 % |
| ductile | 1 | 0 % |
| eng. | 1 | 0 % |
| jeat | 1 | 0 % |
| 1015 | 1 | 0 % |
| karki | 1 | 0 % |
| software | 1 | 0 % |
| maneuvring | 1 | 0 % |
| www.edu116.com | 1 | 0 % |
| parkin | 1 | 0 % |
| solid | 1 | 0 % |
| inner | 1 | 0 % |
| 3th | 1 | 0 % |
| video | 1 | 0 % |
| vektor | 1 | 0 % |
| hopkins | 1 | 0 % |
| henda | 1 | 0 % |
| cav2-001 | 1 | 0 % |
| 357; | 1 | 0 % |
| 415 | 1 | 0 % |
| www.cla-val.com/pdfs/e-cavitation_guide.pdf | 1 | 0 % |
| width | 1 | 0 % |
| measuring | 1 | 0 % |
| advanced | 1 | 0 % |
| good | 1 | 0 % |
| multi-dimensional | 1 | 0 % |
| turbo-pump | 1 | 0 % |
| salty | 1 | 0 % |
| weed | 1 | 0 % |
| influence | 1 | 0 % |
| institute | 1 | 0 % |
| campus | 1 | 0 % |
| cryogenics | 1 | 0 % |
| bubbles | 1 | 0 % |
| max | 1 | 0 % |
| knots | 1 | 0 % |
| state | 1 | 0 % |
| artificial | 1 | 0 % |
| configurations | 1 | 0 % |
| 1 | 1 | 0 % |
| multi-hole | 1 | 0 % |
| step | 1 | 0 % |
| 116 | 1 | 0 % |
| propellors | 1 | 0 % |
| mesh | 1 | 0 % |
| mass | 1 | 0 % |
| b. | 1 | 0 % |
| rayleigh-plesset | 1 | 0 % |
| john | 1 | 0 % |
| similarities | 1 | 0 % |
| skew | 1 | 0 % |
| axial | 1 | 0 % |
| restrction | 1 | 0 % |
| tunnels | 1 | 0 % |
| flat | 1 | 0 % |
| 2.0 | 1 | 0 % |
| liquids | 1 | 0 % |
| nanoparticles | 1 | 0 % |
| hydronautics | 1 | 0 % |
| elbow | 1 | 0 % |
| oxygen | 1 | 0 % |
| roosen | 1 | 0 % |
| bodies | 1 | 0 % |
| lund | 1 | 0 % |
| approximation | 1 | 0 % |
| .n | 1 | 0 % |
| plane | 1 | 0 % |
| burill | 1 | 0 % |
| radius | 1 | 0 % |
| increase | 1 | 0 % |
| deisgn | 1 | 0 % |
| fresh | 1 | 0 % |
| dana | 1 | 0 % |
| p | 1 | 0 % |
| weeks | 1 | 0 % |
| rotor-bearing | 1 | 0 % |
| formed | 1 | 0 % |
| isenthalpic | 1 | 0 % |
| restiction | 1 | 0 % |
| hsieh | 1 | 0 % |
| rider | 1 | 0 % |
| & | 1 | 0 % |
| smooth-sided | 1 | 0 % |
| www.cav2001.library.cateeh.edu.com | 1 | 0 % |
| reentrant | 1 | 0 % |
| rpm | 1 | 0 % |
| lohrberg | 1 | 0 % |
| naca66 | 1 | 0 % |
| thermal | 1 | 0 % |
| formula | 1 | 0 % |
| a; | 1 | 0 % |
| grenoble | 1 | 0 % |
| flow | 1 | 0 % |
| 1993 | 1 | 0 % |
| avoiding | 1 | 0 % |
| princeton | 1 | 0 % |
| laminer | 1 | 0 % |
| sem | 1 | 0 % |
| vibrations | 1 | 0 % |
| savchenko | 1 | 0 % |
| cla-cav | 1 | 0 % |
| horsepower | 1 | 0 % |
| asymmetric | 1 | 0 % |
| meters | 1 | 0 % |
| pipes | 1 | 0 % |
| naval | 1 | 0 % |
| cascade | 1 | 0 % |
| last | 1 | 0 % |
| lecture | 1 | 0 % |
| law | 1 | 0 % |
| soc. | 1 | 0 % |
| historical | 1 | 0 % |
| orifices | 1 | 0 % |
| 1995 | 1 | 0 % |
| parameters | 1 | 0 % |
| profil | 1 | 0 % |
| tension | 1 | 0 % |
| pumpm | 1 | 0 % |
| kaplanturbinen | 1 | 0 % |
| impact | 1 | 0 % |
| xiaolangdi | 1 | 0 % |
| 渦キャビテーション fluent | 1 | 0 % |
| shu | 1 | 0 % |
| arl | 1 | 0 % |
| specification | 1 | 0 % |
| free | 1 | 0 % |
| aisi | 1 | 0 % |
| low | 1 | 0 % |
| polymer | 1 | 0 % |
| disposal | 1 | 0 % |
| surface-piercing | 1 | 0 % |
| pure | 1 | 0 % |
| singhal | 1 | 0 % |
| m | 1 | 0 % |
| sixth | 1 | 0 % |
| okada | 1 | 0 % |
| foil | 1 | 0 % |
| s.a. | 1 | 0 % |
| input | 1 | 0 % |
| missiles | 1 | 0 % |
| molecular | 1 | 0 % |
| seawater | 1 | 0 % |
| 7 | 1 | 0 % |
| maitre | 1 | 0 % |
| milk | 1 | 0 % |
| green | 1 | 0 % |
| eulerian-lagrangian | 1 | 0 % |
| eulerian/lagrangian | 1 | 0 % |
| hess | 1 | 0 % |
| edgedorifice | 1 | 0 % |
| its | 1 | 0 % |
| undersea | 1 | 0 % |
| property | 1 | 0 % |
| loading | 1 | 0 % |
| gotfred | 1 | 0 % |
| similarity | 1 | 0 % |
| surge | 1 | 0 % |
| b | 1 | 0 % |
| ragged | 1 | 0 % |
| multi-orifice | 1 | 0 % |
| function | 1 | 0 % |
| gieseke | 1 | 0 % |
| vulcain | 1 | 0 % |
| linear | 1 | 0 % |
| bearing | 1 | 0 % |
| added | 1 | 0 % |
| books | 1 | 0 % |
| yu | 1 | 0 % |
| fuji | 1 | 0 % |
| rolling | 1 | 0 % |
| 1994 | 1 | 0 % |
| time-frequency | 1 | 0 % |
| techniques | 1 | 0 % |
| lithotripsy | 1 | 0 % |
| struts | 1 | 0 % |
| parson | 1 | 0 % |
| countermasure | 1 | 0 % |
| need | 1 | 0 % |
| dissipation | 1 | 0 % |
| trubopump | 1 | 0 % |
| missile | 1 | 0 % |
| alternating | 1 | 0 % |
| violent | 1 | 0 % |
| ode | 1 | 0 % |
| field | 1 | 0 % |
| location | 1 | 0 % |
| 85000 | 1 | 0 % |
| rebattet | 1 | 0 % |
| estimation | 1 | 0 % |
| cav2d-bl | 1 | 0 % |
| okamura | 1 | 0 % |
| throttle | 1 | 0 % |
| zhong | 1 | 0 % |
| iwano | 1 | 0 % |
| goplan | 1 | 0 % |
| spectron | 1 | 0 % |
| disk | 1 | 0 % |
| window | 1 | 0 % |
| equivalent | 1 | 0 % |
| are | 1 | 0 % |
| cfx | 1 | 0 % |
| center | 1 | 0 % |
| 2b-cfd-g03 | 1 | 0 % |
| . | 1 | 0 % |
| long | 1 | 0 % |
| physical | 1 | 0 % |
| edge | 1 | 0 % |
| inviscid | 1 | 0 % |
| explosion.princeton | 1 | 0 % |
| container | 1 | 0 % |
| laws | 1 | 0 % |
| cryo | 1 | 0 % |
| restrictive | 1 | 0 % |
| handa | 1 | 0 % |
| .abs | 1 | 0 % |
| just | 1 | 0 % |
| measure | 1 | 0 % |
| podded | 1 | 0 % |
| maixner | 1 | 0 % |
| present | 1 | 0 % |
| apparatus.pdf | 1 | 0 % |
| mm | 1 | 0 % |
| thierry | 1 | 0 % |
| parallel | 1 | 0 % |
| conical | 1 | 0 % |
| see | 1 | 0 % |
| jacobian | 1 | 0 % |
| history | 1 | 0 % |
| y. | 1 | 0 % |
| ahmed | 1 | 0 % |
| technology | 1 | 0 % |
| computer | 1 | 0 % |
| ohl | 1 | 0 % |
| accelerometer | 1 | 0 % |
| steady | 1 | 0 % |
| time | 1 | 0 % |
| strength | 1 | 0 % |
| nozzles | 1 | 0 % |
| brennan | 1 | 0 % |
| divergent | 1 | 0 % |
| rar | 1 | 0 % |
| und | 1 | 0 % |
| version | 1 | 0 % |
| image | 1 | 0 % |
| fuel | 1 | 0 % |
| azipods | 1 | 0 % |
| bellmouth | 1 | 0 % |
| lionel | 1 | 0 % |
| vacuum | 1 | 0 % |
| interactions | 1 | 0 % |
| achkinadze | 1 | 0 % |
| 2010 | 1 | 0 % |
| relate | 1 | 0 % |
| alvatore | 1 | 0 % |
| capturing | 1 | 0 % |
| general | 1 | 0 % |
| maximum | 1 | 0 % |
| www | 1 | 0 % |
| 1n | 1 | 0 % |
| restrict | 1 | 0 % |
| mechanisms | 1 | 0 % |
| control | 1 | 0 % |
| nagahara | 1 | 0 % |
| isothermal | 1 | 0 % |
| inks | 1 | 0 % |
| porous | 1 | 0 % |
| tait | 1 | 0 % |
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