| 1397 different keywords | Search | Percent |
|---|
| cavitation | 452 | 7.9 % |
| of | 235 | 4.1 % |
| propeller | 108 | 1.9 % |
| in | 93 | 1.6 % |
| pdf | 90 | 1.5 % |
| orifice | 81 | 1.4 % |
| and | 72 | 1.2 % |
| pump | 67 | 1.1 % |
| a | 64 | 1.1 % |
| vortex | 59 | 1 % |
| flow | 55 | 0.9 % |
| the | 55 | 0.9 % |
| bubble | 54 | 0.9 % |
| fluent | 48 | 0.8 % |
| on | 47 | 0.8 % |
| restriction | 35 | 0.6 % |
| supercavitating | 34 | 0.6 % |
| numerical | 33 | 0.5 % |
| filetype | 33 | 0.5 % |
| pressure | 32 | 0.5 % |
| for | 32 | 0.5 % |
| model | 31 | 0.5 % |
| supercavitation | 31 | 0.5 % |
| centrifugal | 31 | 0.5 % |
| water | 30 | 0.5 % |
| noise | 30 | 0.5 % |
| surface | 29 | 0.5 % |
| cavitating | 29 | 0.5 % |
| erosion | 28 | 0.4 % |
| tip | 28 | 0.4 % |
| experimental | 28 | 0.4 % |
| design | 26 | 0.4 % |
| unsteady | 25 | 0.4 % |
| cavity | 25 | 0.4 % |
| jet | 24 | 0.4 % |
| to | 24 | 0.4 % |
| ship | 24 | 0.4 % |
| rudder | 24 | 0.4 % |
| kaplan | 24 | 0.4 % |
| naca0015 | 23 | 0.4 % |
| analysis | 23 | 0.4 % |
| simulation | 23 | 0.4 % |
| turbine | 21 | 0.3 % |
| effect | 20 | 0.3 % |
| hydrofoil | 19 | 0.3 % |
| propellers | 19 | 0.3 % |
| velocity | 18 | 0.3 % |
| cloud | 18 | 0.3 % |
| pumps | 18 | 0.3 % |
| method | 18 | 0.3 % |
| inducer | 17 | 0.3 % |
| number | 16 | 0.2 % |
| time | 16 | 0.2 % |
| modeling | 16 | 0.2 % |
| prediction | 16 | 0.2 % |
| sheet | 16 | 0.2 % |
| cfd | 16 | 0.2 % |
| frequency | 16 | 0.2 % |
| calculation | 16 | 0.2 % |
| piercing | 16 | 0.2 % |
| study | 15 | 0.2 % |
| with | 15 | 0.2 % |
| motion | 15 | 0.2 % |
| plate | 15 | 0.2 % |
| modelling | 15 | 0.2 % |
| valve | 15 | 0.2 % |
| instability | 14 | 0.2 % |
| bodies | 14 | 0.2 % |
| blade | 14 | 0.2 % |
| boundary | 14 | 0.2 % |
| turbomachinery | 14 | 0.2 % |
| equation | 14 | 0.2 % |
| azipod | 13 | 0.2 % |
| dynamics | 13 | 0.2 % |
| how | 13 | 0.2 % |
| collapse | 12 | 0.2 % |
| flows | 12 | 0.2 % |
| or | 12 | 0.2 % |
| control | 12 | 0.2 % |
| characteristics | 12 | 0.2 % |
| gas | 12 | 0.2 % |
| joint | 12 | 0.2 % |
| nozzle | 12 | 0.2 % |
| horn | 11 | 0.1 % |
| by | 11 | 0.1 % |
| hydrodynamic | 11 | 0.1 % |
| rocket | 11 | 0.1 % |
| using | 11 | 0.1 % |
| partial | 11 | 0.1 % |
| suction | 11 | 0.1 % |
| turbopump | 10 | 0.1 % |
| bubbles | 10 | 0.1 % |
| mass | 10 | 0.1 % |
| liquid | 10 | 0.1 % |
| coefficient | 10 | 0.1 % |
| butterfly | 10 | 0.1 % |
| surge | 10 | 0.1 % |
| theory | 10 | 0.1 % |
| types | 10 | 0.1 % |
| hosangadi | 10 | 0.1 % |
| tunnel | 10 | 0.1 % |
| approach | 10 | 0.1 % |
| orifices | 10 | 0.1 % |
| hydraulic | 10 | 0.1 % |
| supercavity | 10 | 0.1 % |
| high | 10 | 0.1 % |
| symposium | 9 | 0.1 % |
| introduction | 9 | 0.1 % |
| acoustic | 9 | 0.1 % |
| inducers | 9 | 0.1 % |
| ventilated | 9 | 0.1 % |
| naca | 9 | 0.1 % |
| speed | 9 | 0.1 % |
| stability | 9 | 0.1 % |
| mechanism | 9 | 0.1 % |
| two | 9 | 0.1 % |
| diesel | 9 | 0.1 % |
| dynamic | 9 | 0.1 % |
| turbo | 9 | 0.1 % |
| test | 8 | 0.1 % |
| thermal | 8 | 0.1 % |
| an | 8 | 0.1 % |
| impeller | 8 | 0.1 % |
| applications | 8 | 0.1 % |
| cavities | 8 | 0.1 % |
| clearance | 8 | 0.1 % |
| at | 8 | 0.1 % |
| phase | 7 | 0.1 % |
| solid | 7 | 0.1 % |
| intake | 7 | 0.1 % |
| supersonic | 7 | 0.1 % |
| pipe | 7 | 0.1 % |
| behavior | 7 | 0.1 % |
| performance | 7 | 0.1 % |
| y | 7 | 0.1 % |
| paper | 7 | 0.1 % |
| numerical/experimental | 7 | 0.1 % |
| edge | 7 | 0.1 % |
| section | 7 | 0.1 % |
| investigation | 7 | 0.1 % |
| 2d | 7 | 0.1 % |
| near | 7 | 0.1 % |
| measurement | 6 | 0.1 % |
| system | 6 | 0.1 % |
| author | 6 | 0.1 % |
| plates | 6 | 0.1 % |
| injector | 6 | 0.1 % |
| journal | 6 | 0.1 % |
| axial | 6 | 0.1 % |
| vof | 6 | 0.1 % |
| sound | 6 | 0.1 % |
| distribution | 6 | 0.1 % |
| intitle | 6 | 0.1 % |
| stokes | 6 | 0.1 % |
| impact | 6 | 0.1 % |
| added | 6 | 0.1 % |
| bearing | 6 | 0.1 % |
| 3d | 6 | 0.1 % |
| injection | 6 | 0.1 % |
| vibration | 6 | 0.1 % |
| international | 6 | 0.1 % |
| problems | 6 | 0.1 % |
| wave | 6 | 0.1 % |
| methods | 6 | 0.1 % |
| turbulence | 6 | 0.1 % |
| formation | 6 | 0.1 % |
| a. | 6 | 0.1 % |
| watanabe | 6 | 0.1 % |
| condition | 6 | 0.1 % |
| plesset | 6 | 0.1 % |
| nexearch | 6 | 0.1 % |
| experiment | 5 | 0 % |
| fluid | 5 | 0 % |
| avoid | 5 | 0 % |
| drag | 5 | 0 % |
| piping | 5 | 0 % |
| conditions | 5 | 0 % |
| scale | 5 | 0 % |
| formula | 5 | 0 % |
| 2001 | 5 | 0 % |
| prosperetti | 5 | 0 % |
| rapposelli | 5 | 0 % |
| emilio | 5 | 0 % |
| rotating | 5 | 0 % |
| foil | 5 | 0 % |
| distance | 5 | 0 % |
| based | 5 | 0 % |
| some | 5 | 0 % |
| sae | 5 | 0 % |
| e.-a. | 5 | 0 % |
| field | 5 | 0 % |
| s. | 5 | 0 % |
| research | 5 | 0 % |
| between | 5 | 0 % |
| pictures | 5 | 0 % |
| technology | 5 | 0 % |
| discharge | 5 | 0 % |
| upstream | 5 | 0 % |
| engineering | 5 | 0 % |
| behaviour | 5 | 0 % |
| element | 5 | 0 % |
| core | 5 | 0 % |
| m. | 5 | 0 % |
| single | 5 | 0 % |
| .pdf | 5 | 0 % |
| blades | 5 | 0 % |
| university | 5 | 0 % |
| airfoil | 5 | 0 % |
| scott | 5 | 0 % |
| weitendorf | 5 | 0 % |
| gowing | 5 | 0 % |
| machinery | 5 | 0 % |
| abstract | 5 | 0 % |
| inception | 5 | 0 % |
| rayleigh | 5 | 0 % |
| air | 5 | 0 % |
| shapes | 4 | 0 % |
| underwater | 4 | 0 % |
| energy | 4 | 0 % |
| wall | 4 | 0 % |
| super | 4 | 0 % |
| 2-d | 4 | 0 % |
| problem | 4 | 0 % |
| vortices | 4 | 0 % |
| kavitation | 4 | 0 % |
| tsujimoto | 4 | 0 % |
| j | 4 | 0 % |
| occurs | 4 | 0 % |
| radius | 4 | 0 % |
| pit | 4 | 0 % |
| hull | 4 | 0 % |
| analytical | 4 | 0 % |
| panel | 4 | 0 % |
| is | 4 | 0 % |
| patella | 4 | 0 % |
| free | 4 | 0 % |
| papers | 4 | 0 % |
| low | 4 | 0 % |
| jessup | 4 | 0 % |
| b | 4 | 0 % |
| channel | 4 | 0 % |
| angle | 4 | 0 % |
| wake | 4 | 0 % |
| interface | 4 | 0 % |
| are | 4 | 0 % |
| boundaries | 4 | 0 % |
| npsh | 4 | 0 % |
| code | 4 | 0 % |
| vladimir | 4 | 0 % |
| development | 4 | 0 % |
| factor | 4 | 0 % |
| shear | 4 | 0 % |
| tab_hty | 4 | 0 % |
| stage | 4 | 0 % |
| needle | 4 | 0 % |
| new | 4 | 0 % |
| water-entry | 4 | 0 % |
| francis | 4 | 0 % |
| volume | 4 | 0 % |
| mathematical | 4 | 0 % |
| conclusion | 4 | 0 % |
| burrill | 4 | 0 % |
| helium | 4 | 0 % |
| validation | 4 | 0 % |
| region | 4 | 0 % |
| level | 4 | 0 % |
| find | 4 | 0 % |
| leading | 4 | 0 % |
| 1998 | 4 | 0 % |
| submerged | 4 | 0 % |
| photos | 4 | 0 % |
| effects | 4 | 0 % |
| structure | 4 | 0 % |
| particle | 3 | 0 % |
| serebryakov | 3 | 0 % |
| dual | 3 | 0 % |
| calculations | 3 | 0 % |
| equilibrium | 3 | 0 % |
| can | 3 | 0 % |
| type | 3 | 0 % |
| runner | 3 | 0 % |
| proceedings | 3 | 0 % |
| incompressible | 3 | 0 % |
| perspectives | 3 | 0 % |
| explosion | 3 | 0 % |
| density | 3 | 0 % |
| clark | 3 | 0 % |
| submergence | 3 | 0 % |
| source | 3 | 0 % |
| ratio | 3 | 0 % |
| iga | 3 | 0 % |
| observation | 3 | 0 % |
| models | 3 | 0 % |
| ring | 3 | 0 % |
| bell | 3 | 0 % |
| parameter | 3 | 0 % |
| wing | 3 | 0 % |
| oscillation | 3 | 0 % |
| loads | 3 | 0 % |
| spectral | 3 | 0 % |
| fluids | 3 | 0 % |
| delannoy | 3 | 0 % |
| astm | 3 | 0 % |
| index | 3 | 0 % |
| oscillating | 3 | 0 % |
| hydrofoils | 3 | 0 % |
| planing | 3 | 0 % |
| suppression | 3 | 0 % |
| under | 3 | 0 % |
| turbines | 3 | 0 % |
| molecular | 3 | 0 % |
| naca16 | 3 | 0 % |
| measurements | 3 | 0 % |
| spectrometer | 3 | 0 % |
| time-frequency | 3 | 0 % |
| techniques | 3 | 0 % |
| merkle | 3 | 0 % |
| capture | 3 | 0 % |
| fortes | 3 | 0 % |
| engine | 3 | 0 % |
| shape | 3 | 0 % |
| solver | 3 | 0 % |
| damage | 3 | 0 % |
| thornycroft | 3 | 0 % |
| cav2001 | 3 | 0 % |
| force | 3 | 0 % |
| book | 3 | 0 % |
| podded | 3 | 0 % |
| j. | 3 | 0 % |
| re-entrant | 3 | 0 % |
| - | 3 | 0 % |
| generation | 3 | 0 % |
| tank | 3 | 0 % |
| vacuum | 3 | 0 % |
| order | 3 | 0 % |
| multiphase | 3 | 0 % |
| geometry | 3 | 0 % |
| simp. | 3 | 0 % |
| barnaby | 3 | 0 % |
| bem | 3 | 0 % |
| super-cavitating | 3 | 0 % |
| boncinelli | 3 | 0 % |
| kato | 3 | 0 % |
| maneuvering | 3 | 0 % |
| behind | 3 | 0 % |
| shock | 3 | 0 % |
| spray | 3 | 0 % |
| side | 3 | 0 % |
| chahine | 3 | 0 % |
| singularity | 3 | 0 % |
| et | 3 | 0 % |
| downstream | 3 | 0 % |
| transient | 3 | 0 % |
| paolo | 3 | 0 % |
| curvature | 3 | 0 % |
| contour | 3 | 0 % |
| yuka | 3 | 0 % |
| integral | 3 | 0 % |
| han | 3 | 0 % |
| predict | 3 | 0 % |
| induced | 3 | 0 % |
| s | 3 | 0 % |
| proceeding | 3 | 0 % |
| ... | 3 | 0 % |
| instabilities | 3 | 0 % |
| characteristic | 3 | 0 % |
| simple | 3 | 0 % |
| from | 3 | 0 % |
| material | 3 | 0 % |
| ashvin | 3 | 0 % |
| kuklinski | 3 | 0 % |
| straight | 3 | 0 % |
| foils | 3 | 0 % |
| diameter | 3 | 0 % |
| multi | 3 | 0 % |
| form | 2 | 0 % |
| projectile | 2 | 0 % |
| what | 2 | 0 % |
| 587. | 2 | 0 % |
| materials | 2 | 0 % |
| tomita | 2 | 0 % |
| shockwave | 2 | 0 % |
| procedure | 2 | 0 % |
| background | 2 | 0 % |
| rankine | 2 | 0 % |
| predicting | 2 | 0 % |
| kubota | 2 | 0 % |
| isolated | 2 | 0 % |
| non-equilibrium | 2 | 0 % |
| nasa | 2 | 0 % |
| incidence | 2 | 0 % |
| computational | 2 | 0 % |
| obseravtions | 2 | 0 % |
| mech. | 2 | 0 % |
| grid | 2 | 0 % |
| tamura | 2 | 0 % |
| 8 | 2 | 0 % |
| 98 | 2 | 0 % |
| inlet | 2 | 0 % |
| farrell | 2 | 0 % |
| kevin | 2 | 0 % |
| change | 2 | 0 % |
| video | 2 | 0 % |
| henda | 2 | 0 % |
| partially | 2 | 0 % |
| implusive | 2 | 0 % |
| simples | 2 | 0 % |
| sri | 2 | 0 % |
| institute | 2 | 0 % |
| thickness | 2 | 0 % |
| laser | 2 | 0 % |
| pressures | 2 | 0 % |
| yoshiaki | 2 | 0 % |
| ittc | 2 | 0 % |
| max | 2 | 0 % |
| helix | 2 | 0 % |
| slip | 2 | 0 % |
| step | 2 | 0 % |
| mesh | 2 | 0 % |
| rayleigh-plesset | 2 | 0 % |
| propulsors | 2 | 0 % |
| oscillations | 2 | 0 % |
| tunnels | 2 | 0 % |
| liquids | 2 | 0 % |
| pgm | 2 | 0 % |
| chart | 2 | 0 % |
| 1987 | 2 | 0 % |
| rules | 2 | 0 % |
| 1973 | 2 | 0 % |
| 1991 | 2 | 0 % |
| vasin | 2 | 0 % |
| emission | 2 | 0 % |
| kameda | 2 | 0 % |
| formed | 2 | 0 % |
| georges | 2 | 0 % |
| photo | 2 | 0 % |
| reentrant | 2 | 0 % |
| regiane | 2 | 0 % |
| cone | 2 | 0 % |
| sump | 2 | 0 % |
| mccormick | 2 | 0 % |
| small | 2 | 0 % |
| over | 2 | 0 % |
| visualization | 2 | 0 % |
| quality | 2 | 0 % |
| hp | 2 | 0 % |
| g. | 2 | 0 % |
| -citation | 2 | 0 % |
| length | 2 | 0 % |
| notes | 2 | 0 % |
| cavitator | 2 | 0 % |
| raw | 2 | 0 % |
| restricted | 2 | 0 % |
| full-scale | 2 | 0 % |
| template | 2 | 0 % |
| parameters | 2 | 0 % |
| tension | 2 | 0 % |
| restricting | 2 | 0 % |
| asme | 2 | 0 % |
| plant | 2 | 0 % |
| surface-piercing | 2 | 0 % |
| m | 2 | 0 % |
| tuck | 2 | 0 % |
| theoretical | 2 | 0 % |
| djeridi | 2 | 0 % |
| asme-fed | 2 | 0 % |
| streamline | 2 | 0 % |
| propulsion | 2 | 0 % |
| generalized | 2 | 0 % |
| 322–335. | 2 | 0 % |
| inflow | 2 | 0 % |
| vessel | 2 | 0 % |
| ---- | 2 | 0 % |
| acceleration | 2 | 0 % |
| arndt | 2 | 0 % |
| david. | 2 | 0 % |
| treatment | 2 | 0 % |
| kinnas | 2 | 0 % |
| compressible | 2 | 0 % |
| interaction | 2 | 0 % |
| inside | 2 | 0 % |
| stepping | 2 | 0 % |
| phys. | 2 | 0 % |
| expansion | 2 | 0 % |
| transonic | 2 | 0 % |
| application | 2 | 0 % |
| wavelet | 2 | 0 % |
| restrictive | 2 | 0 % |
| department | 2 | 0 % |
| strouhal | 2 | 0 % |
| aluminium | 2 | 0 % |
| olofsson | 2 | 0 % |
| history | 2 | 0 % |
| turbulent | 2 | 0 % |
| g134-95 | 2 | 0 % |
| y. | 2 | 0 % |
| computer | 2 | 0 % |
| attack | 2 | 0 % |
| programming | 2 | 0 % |
| operating | 2 | 0 % |
| levels | 2 | 0 % |
| ’’ | 2 | 0 % |
| resistance | 2 | 0 % |
| azipods | 2 | 0 % |
| shi | 2 | 0 % |
| framework | 2 | 0 % |
| lagrangian | 2 | 0 % |
| 153-158. | 2 | 0 % |
| predictions | 2 | 0 % |
| data | 2 | 0 % |
| coupling | 2 | 0 % |
| petroleum | 2 | 0 % |
| mechanisms | 2 | 0 % |
| ukraine | 2 | 0 % |
| five | 2 | 0 % |
| cp | 2 | 0 % |
| tait | 2 | 0 % |
| spillway | 2 | 0 % |
| jae-moon | 2 | 0 % |
| ‘‘the | 2 | 0 % |
| ultrasound | 2 | 0 % |
| airfoils | 2 | 0 % |
| propella | 2 | 0 % |
| al | 2 | 0 % |
| transport | 2 | 0 % |
| size | 2 | 0 % |
| physics | 2 | 0 % |
| body | 2 | 0 % |
| japikse | 2 | 0 % |
| wageningen | 2 | 0 % |
| hole | 2 | 0 % |
| meter | 2 | 0 % |
| multiple | 2 | 0 % |
| maneuver | 2 | 0 % |
| critical | 2 | 0 % |
| 1996 | 2 | 0 % |
| 222 | 2 | 0 % |
| matsumoto | 2 | 0 % |
| three | 2 | 0 % |
| propeller. | 2 | 0 % |
| jurnal | 2 | 0 % |
| studieson | 2 | 0 % |
| -series | 2 | 0 % |
| principle | 2 | 0 % |
| viscous-inviscid | 2 | 0 % |
| gauge | 2 | 0 % |
| patankar | 2 | 0 % |
| orfice | 2 | 0 % |
| crunch | 2 | 0 % |
| hofmann | 2 | 0 % |
| generator | 2 | 0 % |
| viscous | 2 | 0 % |
| diverging | 2 | 0 % |
| g | 2 | 0 % |
| relative | 2 | 0 % |
| derivation | 2 | 0 % |
| damping | 2 | 0 % |
| ogilvie | 2 | 0 % |
| nomenclature | 2 | 0 % |
| torque | 2 | 0 % |
| forces | 2 | 0 % |
| jean-pierre | 2 | 0 % |
| 2d-curved | 2 | 0 % |
| correction | 2 | 0 % |
| navier | 2 | 0 % |
| 2 | 2 | 0 % |
| 1990 | 2 | 0 % |
| bubbly | 2 | 0 % |
| submarine | 2 | 0 % |
| computation | 2 | 0 % |
| full | 2 | 0 % |
| cav | 2 | 0 % |
| toyo | 2 | 0 % |
| limit | 2 | 0 % |
| processing | 2 | 0 % |
| luminescence | 2 | 0 % |
| phenomena | 2 | 0 % |
| micro | 2 | 0 % |
| spectrum | 2 | 0 % |
| franc | 2 | 0 % |
| minimum | 2 | 0 % |
| v. | 2 | 0 % |
| efficiency | 2 | 0 % |
| grekula | 2 | 0 % |
| shima | 2 | 0 % |
| installation | 2 | 0 % |
| medium | 2 | 0 % |
| blowdown | 2 | 0 % |
| filter | 2 | 0 % |
| homogeneous | 2 | 0 % |
| sea | 2 | 0 % |
| site | 2 | 0 % |
| dynaflow | 2 | 0 % |
| qin | 2 | 0 % |
| mixed-flow | 2 | 0 % |
| l/d | 2 | 0 % |
| advance | 2 | 0 % |
| supercavition | 2 | 0 % |
| f. | 2 | 0 % |
| elliptical | 2 | 0 % |
| picture | 2 | 0 % |
| joint-time-frequency-analysis | 2 | 0 % |
| kueny | 2 | 0 % |
| lucca | 1 | 0 % |
| a.janigro | 1 | 0 % |
| closure | 1 | 0 % |
| ishida | 1 | 0 % |
| charles | 1 | 0 % |
| finite | 1 | 0 % |
| runners. | 1 | 0 % |
| rotation | 1 | 0 % |
| two^phase | 1 | 0 % |
| m3/h | 1 | 0 % |
| light | 1 | 0 % |
| pitting | 1 | 0 % |
| stierman | 1 | 0 % |
| counterjet | 1 | 0 % |
| solids. | 1 | 0 % |
| conclusions | 1 | 0 % |
| threshold | 1 | 0 % |
| marine | 1 | 0 % |
| reduce | 1 | 0 % |
| supercavities | 1 | 0 % |
| part | 1 | 0 % |
| polytropic | 1 | 0 % |
| algebraic | 1 | 0 % |
| 10kc | 1 | 0 % |
| henrik | 1 | 0 % |
| cores | 1 | 0 % |
| buble | 1 | 0 % |
| high-five | 1 | 0 % |
| sauer | 1 | 0 % |
| coefficients | 1 | 0 % |
| dang | 1 | 0 % |
| subsonic | 1 | 0 % |
| panametrics | 1 | 0 % |
| sample | 1 | 0 % |
| sg5 | 1 | 0 % |
| setting | 1 | 0 % |
| resonance | 1 | 0 % |
| hydropower | 1 | 0 % |
| correlation | 1 | 0 % |
| moon | 1 | 0 % |
| rotordynamic | 1 | 0 % |
| inch | 1 | 0 % |
| egusquiza | 1 | 0 % |
| surfaces | 1 | 0 % |
| project | 1 | 0 % |
| astolfi | 1 | 0 % |
| smith | 1 | 0 % |
| mechanics | 1 | 0 % |
| precessing | 1 | 0 % |
| oti-hull | 1 | 0 % |
| karki | 1 | 0 % |
| lc | 1 | 0 % |
| karmen | 1 | 0 % |
| 0.02558 | 1 | 0 % |
| filali | 1 | 0 % |
| niclas | 1 | 0 % |
| transducer | 1 | 0 % |
| numbers | 1 | 0 % |
| taib | 1 | 0 % |
| torus | 1 | 0 % |
| appropriate | 1 | 0 % |
| rate | 1 | 0 % |
| strip | 1 | 0 % |
| pressure-based | 1 | 0 % |
| vapor | 1 | 0 % |
| hopkins | 1 | 0 % |
| nonlifting | 1 | 0 % |
| lift | 1 | 0 % |
| equipment | 1 | 0 % |
| [.0508] | 1 | 0 % |
| k-ε | 1 | 0 % |
| empirical | 1 | 0 % |
| measuring | 1 | 0 % |
| into | 1 | 0 % |
| local | 1 | 0 % |
| level—a | 1 | 0 % |
| μσν | 1 | 0 % |
| making | 1 | 0 % |
| model pressure fluctuation | 1 | 0 % |
| klein | 1 | 0 % |
| 0020 | 1 | 0 % |
| 3% | 1 | 0 % |
| planform | 1 | 0 % |
| ship-skeg | 1 | 0 % |
| near-wall | 1 | 0 % |
| hm3 | 1 | 0 % |
| 1/3 | 1 | 0 % |
| 0012 | 1 | 0 % |
| configurations | 1 | 0 % |
| nuclei | 1 | 0 % |
| pitch | 1 | 0 % |
| sand | 1 | 0 % |
| john | 1 | 0 % |
| show | 1 | 0 % |
| skew | 1 | 0 % |
| de | 1 | 0 % |
| flat | 1 | 0 % |
| multihole | 1 | 0 % |
| associated | 1 | 0 % |
| interference | 1 | 0 % |
| workshop | 1 | 0 % |
| acceptance | 1 | 0 % |
| naca0020 | 1 | 0 % |
| blood | 1 | 0 % |
| fahat | 1 | 0 % |
| duffing | 1 | 0 % |
| facilities | 1 | 0 % |
| duke | 1 | 0 % |
| naca66-012 | 1 | 0 % |
| dimensions | 1 | 0 % |
| & | 1 | 0 % |
| river | 1 | 0 % |
| bar | 1 | 0 % |
| wetted | 1 | 0 % |
| jl | 1 | 0 % |
| due | 1 | 0 % |
| injectors | 1 | 0 % |
| courtot | 1 | 0 % |
| analyzing | 1 | 0 % |
| savchenko | 1 | 0 % |
| hammitt | 1 | 0 % |
| six | 1 | 0 % |
| fixed | 1 | 0 % |
| independent | 1 | 0 % |
| valves. | 1 | 0 % |
| la | 1 | 0 % |
| freestream | 1 | 0 % |
| linearity | 1 | 0 % |
| pei | 1 | 0 % |
| immiscible | 1 | 0 % |
| metz | 1 | 0 % |
| recommended. | 1 | 0 % |
| akamatsu | 1 | 0 % |
| [pdf] | 1 | 0 % |
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