| 1432 different keywords | Search | Percent |
|---|
| cavitation | 511 | 8.7 % |
| of | 141 | 2.4 % |
| pdf | 125 | 2.1 % |
| propeller | 118 | 2 % |
| pump | 105 | 1.7 % |
| in | 82 | 1.4 % |
| orifice | 68 | 1.1 % |
| and | 66 | 1.1 % |
| water | 57 | 0.9 % |
| bubble | 54 | 0.9 % |
| flow | 51 | 0.8 % |
| vortex | 49 | 0.8 % |
| supercavitation | 48 | 0.8 % |
| on | 47 | 0.8 % |
| restriction | 46 | 0.7 % |
| pressure | 45 | 0.7 % |
| the | 44 | 0.7 % |
| analysis | 43 | 0.7 % |
| ship | 42 | 0.7 % |
| fluent | 42 | 0.7 % |
| centrifugal | 42 | 0.7 % |
| noise | 41 | 0.7 % |
| filetype | 40 | 0.6 % |
| numerical | 33 | 0.5 % |
| a | 29 | 0.4 % |
| for | 28 | 0.4 % |
| erosion | 27 | 0.4 % |
| propellers | 27 | 0.4 % |
| model | 26 | 0.4 % |
| design | 25 | 0.4 % |
| xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 24 | 0.4 % |
| method | 24 | 0.4 % |
| hydrofoil | 23 | 0.3 % |
| cavitating | 23 | 0.3 % |
| inducer | 23 | 0.3 % |
| tunnel | 23 | 0.3 % |
| measurement | 22 | 0.3 % |
| & | 22 | 0.3 % |
| cfd | 22 | 0.3 % |
| rudder | 21 | 0.3 % |
| supercavitating | 20 | 0.3 % |
| experimental | 20 | 0.3 % |
| effects | 20 | 0.3 % |
| dynamics | 18 | 0.3 % |
| to | 18 | 0.3 % |
| naca | 18 | 0.3 % |
| cavity | 18 | 0.3 % |
| surface | 17 | 0.2 % |
| how | 17 | 0.2 % |
| unsteady | 17 | 0.2 % |
| blade | 17 | 0.2 % |
| speed | 17 | 0.2 % |
| pumps | 17 | 0.2 % |
| azipod | 16 | 0.2 % |
| fluid | 16 | 0.2 % |
| bubbles | 16 | 0.2 % |
| tip | 16 | 0.2 % |
| cav2001 | 16 | 0.2 % |
| nozzle | 16 | 0.2 % |
| frequency | 16 | 0.2 % |
| phase | 15 | 0.2 % |
| experiment | 15 | 0.2 % |
| theory | 15 | 0.2 % |
| modeling | 15 | 0.2 % |
| vibration | 15 | 0.2 % |
| equation | 15 | 0.2 % |
| joint | 15 | 0.2 % |
| kaplan | 15 | 0.2 % |
| calculation | 15 | 0.2 % |
| drag | 14 | 0.2 % |
| number | 14 | 0.2 % |
| distribution | 14 | 0.2 % |
| turbine | 14 | 0.2 % |
| time | 14 | 0.2 % |
| simulation | 14 | 0.2 % |
| international | 14 | 0.2 % |
| suction | 14 | 0.2 % |
| high | 14 | 0.2 % |
| piercing | 14 | 0.2 % |
| intake | 13 | 0.2 % |
| boundary | 13 | 0.2 % |
| two | 13 | 0.2 % |
| valve | 13 | 0.2 % |
| turbopump | 12 | 0.2 % |
| surge | 12 | 0.2 % |
| by | 11 | 0.1 % |
| symposium | 11 | 0.1 % |
| journal | 11 | 0.1 % |
| jet | 11 | 0.1 % |
| flows | 11 | 0.1 % |
| rocket | 11 | 0.1 % |
| wave | 11 | 0.1 % |
| sheet | 11 | 0.1 % |
| effect | 11 | 0.1 % |
| at | 11 | 0.1 % |
| test | 10 | 0.1 % |
| scale | 10 | 0.1 % |
| coefficient | 10 | 0.1 % |
| hydrodynamic | 10 | 0.1 % |
| modelling | 10 | 0.1 % |
| s | 10 | 0.1 % |
| hydraulic | 10 | 0.1 % |
| supercavity | 10 | 0.1 % |
| sump | 9 | 0.1 % |
| cavitator | 9 | 0.1 % |
| velocity | 9 | 0.1 % |
| are | 9 | 0.1 % |
| mechanism | 9 | 0.1 % |
| prediction | 9 | 0.1 % |
| plesset | 9 | 0.1 % |
| ships | 9 | 0.1 % |
| submerged | 9 | 0.1 % |
| inception | 9 | 0.1 % |
| rayleigh | 9 | 0.1 % |
| marine | 8 | 0.1 % |
| solid | 8 | 0.1 % |
| video | 8 | 0.1 % |
| instability | 8 | 0.1 % |
| liquid | 8 | 0.1 % |
| 2001 | 8 | 0.1 % |
| hydrodynamics | 8 | 0.1 % |
| shock | 8 | 0.1 % |
| characteristics | 8 | 0.1 % |
| helium | 8 | 0.1 % |
| induced | 8 | 0.1 % |
| what | 7 | 0.1 % |
| injector | 7 | 0.1 % |
| de | 7 | 0.1 % |
| performance | 7 | 0.1 % |
| introduction | 7 | 0.1 % |
| butterfly | 7 | 0.1 % |
| rotating | 7 | 0.1 % |
| through | 7 | 0.1 % |
| ventilated | 7 | 0.1 % |
| with | 7 | 0.1 % |
| time-frequency | 7 | 0.1 % |
| hydro | 7 | 0.1 % |
| turbomachinery | 7 | 0.1 % |
| mech | 7 | 0.1 % |
| boncinelli | 7 | 0.1 % |
| cavities | 7 | 0.1 % |
| paolo | 7 | 0.1 % |
| yuan | 7 | 0.1 % |
| equilibrium | 6 | 0.1 % |
| vortices | 6 | 0.1 % |
| study | 6 | 0.1 % |
| laser | 6 | 0.1 % |
| hull | 6 | 0.1 % |
| panel | 6 | 0.1 % |
| is | 6 | 0.1 % |
| jessup | 6 | 0.1 % |
| large | 6 | 0.1 % |
| wake | 6 | 0.1 % |
| types | 6 | 0.1 % |
| edge | 6 | 0.1 % |
| thesis | 6 | 0.1 % |
| tank | 6 | 0.1 % |
| plate | 6 | 0.1 % |
| injection | 6 | 0.1 % |
| impeller | 6 | 0.1 % |
| turbin | 6 | 0.1 % |
| section | 6 | 0.1 % |
| chen | 6 | 0.1 % |
| cloud | 6 | 0.1 % |
| stuart | 6 | 0.1 % |
| dynamic | 6 | 0.1 % |
| turbo | 6 | 0.1 % |
| head | 6 | 0.1 % |
| keller | 6 | 0.1 % |
| homogeneous | 6 | 0.1 % |
| air | 6 | 0.1 % |
| horn | 5 | 0 % |
| super | 5 | 0 % |
| http | 5 | 0 % |
| problem | 5 | 0 % |
| equations | 5 | 0 % |
| piping | 5 | 0 % |
| ratio | 5 | 0 % |
| j | 5 | 0 % |
| mass | 5 | 0 % |
| formed | 5 | 0 % |
| paper | 5 | 0 % |
| stokes | 5 | 0 % |
| acoustic | 5 | 0 % |
| hydrofoils | 5 | 0 % |
| turbines | 5 | 0 % |
| sae | 5 | 0 % |
| angle | 5 | 0 % |
| an | 5 | 0 % |
| treatment | 5 | 0 % |
| damage | 5 | 0 % |
| compressible | 5 | 0 % |
| interaction | 5 | 0 % |
| fortes-patella | 5 | 0 % |
| npsh | 5 | 0 % |
| « | 5 | 0 % |
| code | 5 | 0 % |
| y.tomita | 5 | 0 % |
| kato | 5 | 0 % |
| heister | 5 | 0 % |
| work | 5 | 0 % |
| .pdf | 5 | 0 % |
| venturi | 5 | 0 % |
| steel | 5 | 0 % |
| conference | 5 | 0 % |
| navier | 5 | 0 % |
| bubbly | 5 | 0 % |
| cav | 5 | 0 % |
| partial | 5 | 0 % |
| instabilities | 5 | 0 % |
| around | 5 | 0 % |
| 2d | 5 | 0 % |
| franc | 5 | 0 % |
| abstract | 5 | 0 % |
| towing | 5 | 0 % |
| particles | 5 | 0 % |
| serebryakov | 4 | 0 % |
| underwater | 4 | 0 % |
| thermodynamic | 4 | 0 % |
| ganippa | 4 | 0 % |
| can | 4 | 0 % |
| computational | 4 | 0 % |
| type | 4 | 0 % |
| incompressible | 4 | 0 % |
| structural | 4 | 0 % |
| heat | 4 | 0 % |
| 8 | 4 | 0 % |
| conditions | 4 | 0 % |
| ittc | 4 | 0 % |
| stress | 4 | 0 % |
| bell | 4 | 0 % |
| collapse | 4 | 0 % |
| oscillation | 4 | 0 % |
| technical | 4 | 0 % |
| bar | 4 | 0 % |
| thermal | 4 | 0 % |
| sound | 4 | 0 % |
| due | 4 | 0 % |
| savchenko | 4 | 0 % |
| index | 4 | 0 % |
| oscillating | 4 | 0 % |
| rapposelli | 4 | 0 % |
| emilio | 4 | 0 % |
| impact | 4 | 0 % |
| aisi | 4 | 0 % |
| fluctuation | 4 | 0 % |
| molecular | 4 | 0 % |
| based | 4 | 0 % |
| bearing | 4 | 0 % |
| solution | 4 | 0 % |
| transfer | 4 | 0 % |
| vessel | 4 | 0 % |
| atlar | 4 | 0 % |
| field | 4 | 0 % |
| engine | 4 | 0 % |
| shape | 4 | 0 % |
| pictures | 4 | 0 % |
| j. | 4 | 0 % |
| technology | 4 | 0 % |
| steady | 4 | 0 % |
| multiphase | 4 | 0 % |
| 1984 | 4 | 0 % |
| spillway | 4 | 0 % |
| behaviour | 4 | 0 % |
| element | 4 | 0 % |
| m. | 4 | 0 % |
| turbomachines | 4 | 0 % |
| approach | 4 | 0 % |
| new | 4 | 0 % |
| blades | 4 | 0 % |
| turbulence | 4 | 0 % |
| viscous | 4 | 0 % |
| diesel | 4 | 0 % |
| clearance | 4 | 0 % |
| nomenclature | 4 | 0 % |
| investigation | 4 | 0 % |
| crash | 4 | 0 % |
| computation | 4 | 0 % |
| condition | 4 | 0 % |
| validation | 4 | 0 % |
| from | 4 | 0 % |
| 1055 | 4 | 0 % |
| michel | 4 | 0 % |
| hammer | 4 | 0 % |
| closure | 3 | 0 % |
| atmosphere. | 3 | 0 % |
| projectile | 3 | 0 % |
| particle | 3 | 0 % |
| calculations | 3 | 0 % |
| windsurf | 3 | 0 % |
| smooth | 3 | 0 % |
| scaling | 3 | 0 % |
| wall | 3 | 0 % |
| yuriy | 3 | 0 % |
| euler | 3 | 0 % |
| helical | 3 | 0 % |
| sauer | 3 | 0 % |
| static | 3 | 0 % |
| subsonic | 3 | 0 % |
| converging | 3 | 0 % |
| cav2001_b7.004_n.pdf | 3 | 0 % |
| microbubble | 3 | 0 % |
| vertical | 3 | 0 % |
| 1974 | 3 | 0 % |
| horn-type | 3 | 0 % |
| aluminum | 3 | 0 % |
| stainless | 3 | 0 % |
| flowmeter | 3 | 0 % |
| supersonic | 3 | 0 % |
| 0012 | 3 | 0 % |
| models | 3 | 0 % |
| similarities | 3 | 0 % |
| ring | 3 | 0 % |
| parameter | 3 | 0 % |
| runer | 3 | 0 % |
| 1973 | 3 | 0 % |
| behavior | 3 | 0 % |
| ices | 3 | 0 % |
| photo | 3 | 0 % |
| formula | 3 | 0 % |
| vibrations | 3 | 0 % |
| fluids | 3 | 0 % |
| astm | 3 | 0 % |
| almost | 3 | 0 % |
| 2001. | 3 | 0 % |
| fin | 3 | 0 % |
| acosta | 3 | 0 % |
| valves | 3 | 0 % |
| overview | 3 | 0 % |
| position | 3 | 0 % |
| under | 3 | 0 % |
| discharges | 3 | 0 % |
| developed | 3 | 0 % |
| ballast | 3 | 0 % |
| channel | 3 | 0 % |
| sizing | 3 | 0 % |
| motion | 3 | 0 % |
| shocks | 3 | 0 % |
| arakeri | 3 | 0 % |
| arndt | 3 | 0 % |
| brennen | 3 | 0 % |
| kinnas | 3 | 0 % |
| pod | 3 | 0 % |
| research | 3 | 0 % |
| young | 3 | 0 % |
| . | 3 | 0 % |
| inside | 3 | 0 % |
| physical | 3 | 0 % |
| container | 3 | 0 % |
| 3d | 3 | 0 % |
| power | 3 | 0 % |
| history | 3 | 0 % |
| waves | 3 | 0 % |
| reduction | 3 | 0 % |
| comparison | 3 | 0 % |
| vladimir | 3 | 0 % |
| strength | 3 | 0 % |
| rings | 3 | 0 % |
| sigma | 3 | 0 % |
| yaw | 3 | 0 % |
| formed? | 3 | 0 % |
| data | 3 | 0 % |
| 0015 | 3 | 0 % |
| senocak | 3 | 0 % |
| development | 3 | 0 % |
| spherical | 3 | 0 % |
| callenaere | 3 | 0 % |
| global | 3 | 0 % |
| created | 3 | 0 % |
| shear | 3 | 0 % |
| ultrasound | 3 | 0 % |
| tensile | 3 | 0 % |
| problems | 3 | 0 % |
| applications | 3 | 0 % |
| sessionb3.004 | 3 | 0 % |
| scheme | 3 | 0 % |
| integration | 3 | 0 % |
| supercavitaion | 3 | 0 % |
| hosangadi | 3 | 0 % |
| separation | 3 | 0 % |
| using | 3 | 0 % |
| signal | 3 | 0 % |
| side | 3 | 0 % |
| chahine | 3 | 0 % |
| methods | 3 | 0 % |
| matsumoto | 3 | 0 % |
| volume | 3 | 0 % |
| burrill | 3 | 0 % |
| airfoil | 3 | 0 % |
| temperature | 3 | 0 % |
| area | 3 | 0 % |
| shaft | 3 | 0 % |
| //resolver.caltech.edu/cav2001 | 3 | 0 % |
| orifices | 3 | 0 % |
| farhat | 3 | 0 % |
| labview | 3 | 0 % |
| mean | 3 | 0 % |
| potential | 3 | 0 % |
| lattice | 3 | 0 % |
| kuiper | 3 | 0 % |
| 1978 | 3 | 0 % |
| leading | 3 | 0 % |
| dumont | 3 | 0 % |
| kuklinski | 3 | 0 % |
| photos | 3 | 0 % |
| r | 3 | 0 % |
| barotropic | 3 | 0 % |
| studies | 3 | 0 % |
| stop | 3 | 0 % |
| diameter | 3 | 0 % |
| 206 | 2 | 0 % |
| form | 2 | 0 % |
| rigid | 2 | 0 % |
| karman | 2 | 0 % |
| c.-s. | 2 | 0 % |
| j.e. | 2 | 0 % |
| energy | 2 | 0 % |
| hem | 2 | 0 % |
| author | 2 | 0 % |
| incipient | 2 | 0 % |
| shockwave | 2 | 0 % |
| bernoulli | 2 | 0 % |
| developments | 2 | 0 % |
| procedure | 2 | 0 % |
| ikohagi | 2 | 0 % |
| froude | 2 | 0 % |
| t. | 2 | 0 % |
| analyzer | 2 | 0 % |
| incidence | 2 | 0 % |
| cross-section | 2 | 0 % |
| lindau | 2 | 0 % |
| navier-stokes | 2 | 0 % |
| circulating | 2 | 0 % |
| viscosity | 2 | 0 % |
| hydrocode | 2 | 0 % |
| venkateswaran | 2 | 0 % |
| terms | 2 | 0 % |
| attached | 2 | 0 % |
| industrial | 2 | 0 % |
| knapp | 2 | 0 % |
| camber | 2 | 0 % |
| npl | 2 | 0 % |
| andersson | 2 | 0 % |
| oti-hull | 2 | 0 % |
| component | 2 | 0 % |
| lc | 2 | 0 % |
| fast | 2 | 0 % |
| sometimes | 2 | 0 % |
| analyses | 2 | 0 % |
| vapor | 2 | 0 % |
| change | 2 | 0 % |
| partially | 2 | 0 % |
| revolution | 2 | 0 % |
| source | 2 | 0 % |
| discrete | 2 | 0 % |
| mouth | 2 | 0 % |
| influence | 2 | 0 % |
| pipe | 2 | 0 % |
| slip | 2 | 0 % |
| artificial | 2 | 0 % |
| nuclei | 2 | 0 % |
| step | 2 | 0 % |
| propellors | 2 | 0 % |
| pitch | 2 | 0 % |
| about | 2 | 0 % |
| r. | 2 | 0 % |
| sname | 2 | 0 % |
| bodies | 2 | 0 % |
| radius | 2 | 0 % |
| blood | 2 | 0 % |
| georges | 2 | 0 % |
| file | 2 | 0 % |
| naca66 | 2 | 0 % |
| fine | 2 | 0 % |
| grenoble | 2 | 0 % |
| cone | 2 | 0 % |
| kerwin | 2 | 0 % |
| nonlinear | 2 | 0 % |
| monitoring | 2 | 0 % |
| small | 2 | 0 % |
| six | 2 | 0 % |
| la | 2 | 0 % |
| newcastle | 2 | 0 % |
| operation | 2 | 0 % |
| naval | 2 | 0 % |
| “ | 2 | 0 % |
| cascade | 2 | 0 % |
| g. | 2 | 0 % |
| notes | 2 | 0 % |
| 1980 | 2 | 0 % |
| law | 2 | 0 % |
| two-phase | 2 | 0 % |
| j.m. | 2 | 0 % |
| propellor | 2 | 0 % |
| restricting | 2 | 0 % |
| asme | 2 | 0 % |
| free | 2 | 0 % |
| factory | 2 | 0 % |
| industry | 2 | 0 % |
| tuck | 2 | 0 % |
| constantinescu | 2 | 0 % |
| theoretical | 2 | 0 % |
| rise | 2 | 0 % |
| brix | 2 | 0 % |
| runge | 2 | 0 % |
| gotfred | 2 | 0 % |
| inducers | 2 | 0 % |
| francesco | 2 | 0 % |
| sasajima | 2 | 0 % |
| layer | 2 | 0 % |
| some | 2 | 0 % |
| function | 2 | 0 % |
| vulcain | 2 | 0 % |
| kirchner | 2 | 0 % |
| propulsion | 2 | 0 % |
| set | 2 | 0 % |
| vogel | 2 | 0 % |
| spot | 2 | 0 % |
| lithotripsy | 2 | 0 % |
| berntsen | 2 | 0 % |
| david | 2 | 0 % |
| stft | 2 | 0 % |
| bvp | 2 | 0 % |
| does | 2 | 0 % |
| cavatation | 2 | 0 % |
| process | 2 | 0 % |
| s. | 2 | 0 % |
| intakes | 2 | 0 % |
| tab_sug | 2 | 0 % |
| photographs | 2 | 0 % |
| naca0012 | 2 | 0 % |
| book | 2 | 0 % |
| phenomenon | 2 | 0 % |
| pilipenko | 2 | 0 % |
| cruise | 2 | 0 % |
| conical | 2 | 0 % |
| salvatore | 2 | 0 % |
| cav2001sessionb3.006 | 2 | 0 % |
| y. | 2 | 0 % |
| attack | 2 | 0 % |
| nozzles | 2 | 0 % |
| transactions | 2 | 0 % |
| 2000 | 2 | 0 % |
| operating | 2 | 0 % |
| zero | 2 | 0 % |
| levels | 2 | 0 % |
| image | 2 | 0 % |
| torsion | 2 | 0 % |
| generation | 2 | 0 % |
| fft | 2 | 0 % |
| transients | 2 | 0 % |
| bellmouth | 2 | 0 % |
| kalumuck | 2 | 0 % |
| timm | 2 | 0 % |
| lionel | 2 | 0 % |
| diagram | 2 | 0 % |
| two-dimensional | 2 | 0 % |
| values | 2 | 0 % |
| impellers | 2 | 0 % |
| votex | 2 | 0 % |
| manoeuvring | 2 | 0 % |
| cp | 2 | 0 % |
| yoichiro | 2 | 0 % |
| hemispherical | 2 | 0 % |
| mit | 2 | 0 % |
| manual | 2 | 0 % |
| axisymmetric | 2 | 0 % |
| maneuvering | 2 | 0 % |
| geometrical | 2 | 0 % |
| engineering | 2 | 0 % |
| japikse | 2 | 0 % |
| à | 2 | 0 % |
| incipent | 2 | 0 % |
| mécanismes | 2 | 0 % |
| mod | 2 | 0 % |
| rudders | 2 | 0 % |
| components | 2 | 0 % |
| critical | 2 | 0 % |
| smoothing | 2 | 0 % |
| l’étude | 2 | 0 % |
| t | 2 | 0 % |
| throat | 2 | 0 % |
| designs | 2 | 0 % |
| other | 2 | 0 % |
| propeller-hull | 2 | 0 % |
| coating | 2 | 0 % |
| simulations | 2 | 0 % |
| reference | 2 | 0 % |
| fourth | 2 | 0 % |
| university | 2 | 0 % |
| sato | 2 | 0 % |
| nose | 2 | 0 % |
| eulerian/lagrangian | 2 | 0 % |
| patankar | 2 | 0 % |
| delale | 2 | 0 % |
| results | 2 | 0 % |
| kutta | 2 | 0 % |
| lubrication | 2 | 0 % |
| three-dimensional | 2 | 0 % |
| damping | 2 | 0 % |
| ogilvie | 2 | 0 % |
| lifting-surface | 2 | 0 % |
| logvinovich | 2 | 0 % |
| gas | 2 | 0 % |
| delale/ | 2 | 0 % |
| forms | 2 | 0 % |
| nicolas | 2 | 0 % |
| scott | 2 | 0 % |
| integral | 2 | 0 % |
| shyy | 2 | 0 % |
| throttling | 2 | 0 % |
| schnerr | 2 | 0 % |
| mixed | 2 | 0 % |
| profile | 2 | 0 % |
| jules | 2 | 0 % |
| a.j. | 2 | 0 % |
| thrust | 2 | 0 % |
| a. | 2 | 0 % |
| soft | 2 | 0 % |
| a.cavitation | 2 | 0 % |
| imaging | 2 | 0 % |
| criteria | 2 | 0 % |
| contribution | 2 | 0 % |
| curve | 2 | 0 % |
| mastumoto | 2 | 0 % |
| full | 2 | 0 % |
| lauterborn | 2 | 0 % |
| pgm-10kc | 2 | 0 % |
| gowing | 2 | 0 % |
| adiabatic | 2 | 0 % |
| j.p. | 2 | 0 % |
| efficient | 2 | 0 % |
| definition | 2 | 0 % |
| i | 2 | 0 % |
| quasi-static | 2 | 0 % |
| l‘érosion | 2 | 0 % |
| coordinates | 2 | 0 % |
| micro | 2 | 0 % |
| machinery | 2 | 0 % |
| vortexes | 2 | 0 % |
| characteristic | 2 | 0 % |
| spectrum | 2 | 0 % |
| edu | 2 | 0 % |
| level | 2 | 0 % |
| outflow | 2 | 0 % |
| coupled | 2 | 0 % |
| swl | 2 | 0 % |
| efficiency | 2 | 0 % |
| chomiak | 2 | 0 % |
| walther | 2 | 0 % |
| site | 2 | 0 % |
| 66 | 2 | 0 % |
| robert | 2 | 0 % |
| vortical | 2 | 0 % |
| counter | 2 | 0 % |
| lee | 2 | 0 % |
| material | 2 | 0 % |
| ashvin | 2 | 0 % |
| dns | 2 | 0 % |
| cross | 2 | 0 % |
| schmidt | 2 | 0 % |
| near | 2 | 0 % |
| calculate | 2 | 0 % |
| report | 2 | 0 % |
| advance | 2 | 0 % |
| ce | 2 | 0 % |
| h | 2 | 0 % |
| picture | 2 | 0 % |
| l. | 2 | 0 % |
| nexearch | 2 | 0 % |
| storm | 1 | 0 % |
| harp | 1 | 0 % |
| implementation | 1 | 0 % |
| proportion | 1 | 0 % |
| quaternion | 1 | 0 % |
| visualizations | 1 | 0 % |
| rotation | 1 | 0 % |
| reasons | 1 | 0 % |
| constrained | 1 | 0 % |
| aiaa | 1 | 0 % |
| stepanoff | 1 | 0 % |
| yu.n. | 1 | 0 % |
| electromagnetic | 1 | 0 % |
| direction | 1 | 0 % |
| //cav2001.library.caltech.edu/319/00/a9.006.pdf | 1 | 0 % |
| reduce | 1 | 0 % |
| skin | 1 | 0 % |
| sv | 1 | 0 % |
| vessels | 1 | 0 % |
| journees | 1 | 0 % |
| 1969 | 1 | 0 % |
| part | 1 | 0 % |
| polytropic | 1 | 0 % |
| curves | 1 | 0 % |
| carolyn | 1 | 0 % |
| qian | 1 | 0 % |
| kubota | 1 | 0 % |
| coefficients | 1 | 0 % |
| hydrogen | 1 | 0 % |
| 3525 | 1 | 0 % |
| circular-cylindrical | 1 | 0 % |
| sample | 1 | 0 % |
| very | 1 | 0 % |
| 950290 | 1 | 0 % |
| hydropower | 1 | 0 % |
| ntnu | 1 | 0 % |
| shin | 1 | 0 % |
| gates | 1 | 0 % |
| 2-d | 1 | 0 % |
| runner | 1 | 0 % |
| photons | 1 | 0 % |
| estimate | 1 | 0 % |
| smith | 1 | 0 % |
| check | 1 | 0 % |
| m/s | 1 | 0 % |
| cofficient | 1 | 0 % |
| grid | 1 | 0 % |
| mohamed | 1 | 0 % |
| avoid | 1 | 0 % |
| eye | 1 | 0 % |
| inlet | 1 | 0 % |
| ? | 1 | 0 % |
| transducer | 1 | 0 % |
| excitation | 1 | 0 % |
| taib | 1 | 0 % |
| james | 1 | 0 % |
| rate | 1 | 0 % |
| race | 1 | 0 % |
| explosion | 1 | 0 % |
| implicit | 1 | 0 % |
| disturb | 1 | 0 % |
| density | 1 | 0 % |
| lift | 1 | 0 % |
| top | 1 | 0 % |
| naca0015 | 1 | 0 % |
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| //journals.cambridge.org/article_s0022112002007784 | 1 | 0 % |
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| <xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 1 | 0 % |
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| Other words | 432 | 7.3 % |