| 171 different keywords | Search | Percent |
|---|
| cavitation | 24 | 7.5 % |
| of | 18 | 5.6 % |
| vortex | 9 | 2.8 % |
| and | 7 | 2.2 % |
| model | 5 | 1.5 % |
| supercavitation | 5 | 1.5 % |
| in | 5 | 1.5 % |
| xxxñ | 5 | 1.5 % |
| submerged | 5 | 1.5 % |
| effects | 5 | 1.5 % |
| orifice | 5 | 1.5 % |
| pdf | 4 | 1.2 % |
| method | 4 | 1.2 % |
| pump | 4 | 1.2 % |
| inducer | 3 | 0.9 % |
| 2001 | 3 | 0.9 % |
| propeller | 3 | 0.9 % |
| stream | 3 | 0.9 % |
| free | 3 | 0.9 % |
| size | 3 | 0.9 % |
| large-eddy | 3 | 0.9 % |
| bubble | 3 | 0.9 % |
| the | 3 | 0.9 % |
| nuclei | 3 | 0.9 % |
| mos | 2 | 0.6 % |
| ville | 2 | 0.6 % |
| scaling | 2 | 0.6 % |
| attack | 2 | 0.6 % |
| characterization | 2 | 0.6 % |
| panel | 2 | 0.6 % |
| disadvantages | 2 | 0.6 % |
| index | 2 | 0.6 % |
| helical | 2 | 0.6 % |
| les | 2 | 0.6 % |
| flop | 2 | 0.6 % |
| acoustic | 2 | 0.6 % |
| filetype | 2 | 0.6 % |
| fluent | 2 | 0.6 % |
| suction | 2 | 0.6 % |
| downsampling | 2 | 0.6 % |
| simulation | 2 | 0.6 % |
| wigner | 2 | 0.6 % |
| on | 2 | 0.6 % |
| concerning | 2 | 0.6 % |
| applications | 2 | 0.6 % |
| flip | 2 | 0.6 % |
| cavity | 2 | 0.6 % |
| synchronizer | 2 | 0.6 % |
| angle | 2 | 0.6 % |
| hysteresis | 2 | 0.6 % |
| instability | 2 | 0.6 % |
| artificial | 2 | 0.6 % |
| r. | 2 | 0.6 % |
| questions | 2 | 0.6 % |
| calculation | 2 | 0.6 % |
| inception | 2 | 0.6 % |
| simulations | 2 | 0.6 % |
| inherent | 2 | 0.6 % |
| restriction | 2 | 0.6 % |
| performance | 2 | 0.6 % |
| eulerian | 1 | 0.3 % |
| conical | 1 | 0.3 % |
| “boundaryintegral | 1 | 0.3 % |
| stall | 1 | 0.3 % |
| flow | 1 | 0.3 % |
| turbulent | 1 | 0.3 % |
| j. | 1 | 0.3 % |
| formation | 1 | 0.3 % |
| dynamic | 1 | 0.3 % |
| hull | 1 | 0.3 % |
| -4 | 1 | 0.3 % |
| reduction | 1 | 0.3 % |
| ship | 1 | 0.3 % |
| numerical | 1 | 0.3 % |
| vibrations | 1 | 0.3 % |
| technology | 1 | 0.3 % |
| spool | 1 | 0.3 % |
| turbopump | 1 | 0.3 % |
| gas | 1 | 0.3 % |
| variable | 1 | 0.3 % |
| area | 1 | 0.3 % |
| steady | 1 | 0.3 % |
| flashing | 1 | 0.3 % |
| incipient | 1 | 0.3 % |
| phase | 1 | 0.3 % |
| erosion | 1 | 0.3 % |
| 4th | 1 | 0.3 % |
| cascade | 1 | 0.3 % |
| pasadena | 1 | 0.3 % |
| otto | 1 | 0.3 % |
| butterfly | 1 | 0.3 % |
| p. | 1 | 0.3 % |
| a. | 1 | 0.3 % |
| m_lg | 1 | 0.3 % |
| helium | 1 | 0.3 % |
| plate | 1 | 0.3 % |
| fluid | 1 | 0.3 % |
| calculatio | 1 | 0.3 % |
| valve | 1 | 0.3 % |
| criteria | 1 | 0.3 % |
| lagrangian | 1 | 0.3 % |
| visual | 1 | 0.3 % |
| ” | 1 | 0.3 % |
| by | 1 | 0.3 % |
| bb2b6177df83aba8c39a609958cfef04 | 1 | 0.3 % |
| rotating | 1 | 0.3 % |
| nearboundaries | 1 | 0.3 % |
| 1986 | 1 | 0.3 % |
| blade | 1 | 0.3 % |
| algorithms | 1 | 0.3 % |
| hulls | 1 | 0.3 % |
| spherical | 1 | 0.3 % |
| incompressible | 1 | 0.3 % |
| hierarchical | 1 | 0.3 % |
| torpedo | 1 | 0.3 % |
| paperuri | 1 | 0.3 % |
| dynamics | 1 | 0.3 % |
| grid | 1 | 0.3 % |
| software | 1 | 0.3 % |
| inlet | 1 | 0.3 % |
| andreas | 1 | 0.3 % |
| axisymmetric | 1 | 0.3 % |
| drag | 1 | 0.3 % |
| hess | 1 | 0.3 % |
| line | 1 | 0.3 % |
| keller | 1 | 0.3 % |
| determined | 1 | 0.3 % |
| vlsi | 1 | 0.3 % |
| coupled | 1 | 0.3 % |
| tanguay | 1 | 0.3 % |
| number | 1 | 0.3 % |
| california | 1 | 0.3 % |
| shock | 1 | 0.3 % |
| added | 1 | 0.3 % |
| grid-independent | 1 | 0.3 % |
| symposium | 1 | 0.3 % |
| meaning | 1 | 0.3 % |
| advantages | 1 | 0.3 % |
| ten | 1 | 0.3 % |
| design | 1 | 0.3 % |
| characteristics | 1 | 0.3 % |
| recurrences | 1 | 0.3 % |
| institute | 1 | 0.3 % |
| usa. | 1 | 0.3 % |
| int. | 1 | 0.3 % |
| using | 1 | 0.3 % |
| tunnel | 1 | 0.3 % |
| meter | 1 | 0.3 % |
| bubbles | 1 | 0.3 % |
| pearson | 1 | 0.3 % |
| an | 1 | 0.3 % |
| mass | 1 | 0.3 % |
| methods | 1 | 0.3 % |
| sqcm | 1 | 0.3 % |
| for | 1 | 0.3 % |
| occurred | 1 | 0.3 % |
| supercavitating | 1 | 0.3 % |
| chimera | 1 | 0.3 % |
| s. | 1 | 0.3 % |
| diffusion | 1 | 0.3 % |
| blake | 1 | 0.3 % |
| impella | 1 | 0.3 % |
| brewe | 1 | 0.3 % |
| turbulentten | 1 | 0.3 % |
| centrifugal | 1 | 0.3 % |
| cav2001 | 1 | 0.3 % |
| unsteady | 1 | 0.3 % |
| behavior | 1 | 0.3 % |
| force | 1 | 0.3 % |
| structure | 1 | 0.3 % |
| air | 1 | 0.3 % |
|