1539 different keywords | Search | Percent |
cavitation | 574 | 8.9 % |
of | 196 | 3 % |
pdf | 155 | 2.4 % |
in | 109 | 1.6 % |
propeller | 106 | 1.6 % |
pump | 103 | 1.6 % |
orifice | 80 | 1.2 % |
and | 71 | 1.1 % |
water | 68 | 1 % |
flow | 62 | 0.9 % |
bubble | 61 | 0.9 % |
vortex | 60 | 0.9 % |
a | 56 | 0.8 % |
centrifugal | 55 | 0.8 % |
fluent | 54 | 0.8 % |
pressure | 53 | 0.8 % |
the | 46 | 0.7 % |
filetype | 45 | 0.7 % |
on | 43 | 0.6 % |
restriction | 42 | 0.6 % |
for | 41 | 0.6 % |
erosion | 40 | 0.6 % |
numerical | 37 | 0.5 % |
turbine | 37 | 0.5 % |
cavitating | 34 | 0.5 % |
model | 33 | 0.5 % |
design | 33 | 0.5 % |
method | 31 | 0.4 % |
surface | 30 | 0.4 % |
jet | 30 | 0.4 % |
simulation | 30 | 0.4 % |
kaplan | 30 | 0.4 % |
analysis | 29 | 0.4 % |
supercavitation | 29 | 0.4 % |
noise | 28 | 0.4 % |
xxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxxx | 27 | 0.4 % |
tunnel | 24 | 0.3 % |
number | 23 | 0.3 % |
pumps | 23 | 0.3 % |
ship | 23 | 0.3 % |
unsteady | 22 | 0.3 % |
blade | 22 | 0.3 % |
turbomachinery | 22 | 0.3 % |
propellers | 22 | 0.3 % |
effect | 22 | 0.3 % |
bubbles | 20 | 0.3 % |
test | 20 | 0.3 % |
& | 20 | 0.3 % |
hydrofoil | 20 | 0.3 % |
by | 19 | 0.2 % |
wave | 19 | 0.2 % |
calculation | 19 | 0.2 % |
study | 18 | 0.2 % |
tip | 18 | 0.2 % |
to | 18 | 0.2 % |
cfd | 18 | 0.2 % |
experimental | 18 | 0.2 % |
azipod | 17 | 0.2 % |
modeling | 17 | 0.2 % |
equation | 17 | 0.2 % |
liquid | 16 | 0.2 % |
cav2001 | 15 | 0.2 % |
inducer | 15 | 0.2 % |
speed | 15 | 0.2 % |
suction | 15 | 0.2 % |
nozzle | 15 | 0.2 % |
frequency | 15 | 0.2 % |
dynamics | 14 | 0.2 % |
flows | 14 | 0.2 % |
types | 14 | 0.2 % |
diesel | 14 | 0.2 % |
rudder | 14 | 0.2 % |
coefficient | 13 | 0.2 % |
boundary | 13 | 0.2 % |
induced | 13 | 0.2 % |
super | 12 | 0.1 % |
with | 12 | 0.1 % |
shock | 12 | 0.1 % |
orifices | 12 | 0.1 % |
piercing | 12 | 0.1 % |
author | 11 | 0.1 % |
fluid | 11 | 0.1 % |
emission | 11 | 0.1 % |
performance | 11 | 0.1 % |
free | 11 | 0.1 % |
investigation | 11 | 0.1 % |
modelling | 11 | 0.1 % |
valve | 11 | 0.1 % |
cav | 11 | 0.1 % |
joint | 11 | 0.1 % |
video | 10 | 0.1 % |
symposium | 10 | 0.1 % |
laser | 10 | 0.1 % |
pipe | 10 | 0.1 % |
intitle | 10 | 0.1 % |
acoustic | 10 | 0.1 % |
rocket | 10 | 0.1 % |
impeller | 10 | 0.1 % |
characteristics | 10 | 0.1 % |
using | 10 | 0.1 % |
.pdf | 10 | 0.1 % |
rayleigh | 10 | 0.1 % |
high | 10 | 0.1 % |
effects | 10 | 0.1 % |
experiment | 9 | 0.1 % |
stokes | 9 | 0.1 % |
velocity | 9 | 0.1 % |
naca | 9 | 0.1 % |
size | 9 | 0.1 % |
cavity | 9 | 0.1 % |
navier | 9 | 0.1 % |
phenomena | 9 | 0.1 % |
measurement | 8 | 0.1 % |
marine | 8 | 0.1 % |
drag | 8 | 0.1 % |
intake | 8 | 0.1 % |
how | 8 | 0.1 % |
collapse | 8 | 0.1 % |
formula | 8 | 0.1 % |
sound | 8 | 0.1 % |
hull | 8 | 0.1 % |
2001 | 8 | 0.1 % |
distribution | 8 | 0.1 % |
cavitator | 8 | 0.1 % |
low | 8 | 0.1 % |
supercavitating | 8 | 0.1 % |
code | 8 | 0.1 % |
multiphase | 8 | 0.1 % |
international | 8 | 0.1 % |
sheet | 8 | 0.1 % |
2d | 8 | 0.1 % |
kuklinski | 8 | 0.1 % |
system | 7 | 0.1 % |
phase | 7 | 0.1 % |
rate | 7 | 0.1 % |
piping | 7 | 0.1 % |
is | 7 | 0.1 % |
paper | 7 | 0.1 % |
butterfly | 7 | 0.1 % |
two-phase | 7 | 0.1 % |
added | 7 | 0.1 % |
time-frequency | 7 | 0.1 % |
merkle | 7 | 0.1 % |
theory | 7 | 0.1 % |
edge | 7 | 0.1 % |
between | 7 | 0.1 % |
force | 7 | 0.1 % |
time | 7 | 0.1 % |
diagram | 7 | 0.1 % |
vibration | 7 | 0.1 % |
tab_hty | 7 | 0.1 % |
single | 7 | 0.1 % |
dynamic | 7 | 0.1 % |
hydraulic | 7 | 0.1 % |
submerged | 7 | 0.1 % |
particle | 6 | 0 % |
what | 6 | 0 % |
turbopump | 6 | 0 % |
horn | 6 | 0 % |
energy | 6 | 0 % |
navier-stokes | 6 | 0 % |
solid | 6 | 0 % |
lift | 6 | 0 % |
injector | 6 | 0 % |
mass | 6 | 0 % |
ahuja | 6 | 0 % |
ring | 6 | 0 % |
scale | 6 | 0 % |
technical | 6 | 0 % |
reentrant | 6 | 0 % |
introduction | 6 | 0 % |
hydrodynamics | 6 | 0 % |
rapposelli | 6 | 0 % |
emilio | 6 | 0 % |
hydrodynamic | 6 | 0 % |
oil | 6 | 0 % |
sae | 6 | 0 % |
atlar | 6 | 0 % |
field | 6 | 0 % |
damage | 6 | 0 % |
diatomic | 6 | 0 % |
npsh | 6 | 0 % |
strength | 6 | 0 % |
injection | 6 | 0 % |
ultrasound | 6 | 0 % |
body | 6 | 0 % |
methods | 6 | 0 % |
two | 6 | 0 % |
... | 6 | 0 % |
luminescence | 6 | 0 % |
plesset | 6 | 0 % |
ships | 6 | 0 % |
kjeldsen | 6 | 0 % |
robert | 6 | 0 % |
nexearch | 6 | 0 % |
type | 5 | 0 % |
runner | 5 | 0 % |
incompressible | 5 | 0 % |
mohamed | 5 | 0 % |
ratio | 5 | 0 % |
artificial | 5 | 0 % |
oscillation | 5 | 0 % |
eulerian | 5 | 0 % |
due | 5 | 0 % |
savchenko | 5 | 0 % |
astm | 5 | 0 % |
hydrofoils | 5 | 0 % |
tension | 5 | 0 % |
rotating | 5 | 0 % |
layer | 5 | 0 % |
ventilated | 5 | 0 % |
engine | 5 | 0 % |
reynolds | 5 | 0 % |
application | 5 | 0 % |
experiments | 5 | 0 % |
3d | 5 | 0 % |
strouhal | 5 | 0 % |
reduction | 5 | 0 % |
technology | 5 | 0 % |
vladimir | 5 | 0 % |
turbopumps | 5 | 0 % |
thesis | 5 | 0 % |
plate | 5 | 0 % |
geometry | 5 | 0 % |
data | 5 | 0 % |
mechanism | 5 | 0 % |
spherical | 5 | 0 % |
wageningen | 5 | 0 % |
compressibility | 5 | 0 % |
transient | 5 | 0 % |
prediction | 5 | 0 % |
turbo | 5 | 0 % |
farhat | 5 | 0 % |
rarefaction | 5 | 0 % |
testing | 5 | 0 % |
micro | 5 | 0 % |
spectrum | 5 | 0 % |
meridional | 5 | 0 % |
inception | 5 | 0 % |
barotropic | 5 | 0 % |
picture | 5 | 0 % |
serebryakov | 4 | 0 % |
calculations | 4 | 0 % |
equilibrium | 4 | 0 % |
scaling | 4 | 0 % |
turning | 4 | 0 % |
sauer | 4 | 0 % |
ductile | 4 | 0 % |
software | 4 | 0 % |
tsujimoto | 4 | 0 % |
supersonic | 4 | 0 % |
instability | 4 | 0 % |
nuclei | 4 | 0 % |
bell | 4 | 0 % |
quasi-3d | 4 | 0 % |
thermal | 4 | 0 % |
grenoble | 4 | 0 % |
sump | 4 | 0 % |
turbomachine | 4 | 0 % |
template | 4 | 0 % |
stoke | 4 | 0 % |
asme | 4 | 0 % |
papers | 4 | 0 % |
gotfred | 4 | 0 % |
rans | 4 | 0 % |
berntsen | 4 | 0 % |
lithotripsy | 4 | 0 % |
an | 4 | 0 % |
does | 4 | 0 % |
compressible | 4 | 0 % |
tullis | 4 | 0 % |
turbulent | 4 | 0 % |
cp | 4 | 0 % |
maneuvering | 4 | 0 % |
problems | 4 | 0 % |
tensile | 4 | 0 % |
difference | 4 | 0 % |
element | 4 | 0 % |
specific | 4 | 0 % |
side | 4 | 0 % |
meter | 4 | 0 % |
technologies | 4 | 0 % |
critical | 4 | 0 % |
gap | 4 | 0 % |
new | 4 | 0 % |
curved | 4 | 0 % |
blades | 4 | 0 % |
volume | 4 | 0 % |
min | 4 | 0 % |
backward | 4 | 0 % |
viscous | 4 | 0 % |
technique | 4 | 0 % |
forces | 4 | 0 % |
crash | 4 | 0 % |
computation | 4 | 0 % |
head | 4 | 0 % |
curve | 4 | 0 % |
keller | 4 | 0 % |
level | 4 | 0 % |
from | 4 | 0 % |
homogeneous | 4 | 0 % |
material | 4 | 0 % |
standard | 4 | 0 % |
michel | 4 | 0 % |
song | 4 | 0 % |
r | 4 | 0 % |
at | 4 | 0 % |
stop | 4 | 0 % |
structure | 4 | 0 % |
air | 4 | 0 % |
load | 3 | 0 % |
underwater | 3 | 0 % |
materials | 3 | 0 % |
molecule | 3 | 0 % |
fraction | 3 | 0 % |
dir | 3 | 0 % |
schaffar | 3 | 0 % |
prop | 3 | 0 % |
helical | 3 | 0 % |
trailing | 3 | 0 % |
moving | 3 | 0 % |
grid | 3 | 0 % |
tamura | 3 | 0 % |
heat | 3 | 0 % |
inlet | 3 | 0 % |
focusing | 3 | 0 % |
revolution | 3 | 0 % |
density | 3 | 0 % |
hydrauliques | 3 | 0 % |
mouth | 3 | 0 % |
journal | 3 | 0 % |
influence | 3 | 0 % |
institute | 3 | 0 % |
pressures | 3 | 0 % |
yoshiaki | 3 | 0 % |
facing | 3 | 0 % |
slip | 3 | 0 % |
state | 3 | 0 % |
fluctuations | 3 | 0 % |
step | 3 | 0 % |
mesh | 3 | 0 % |
vof | 3 | 0 % |
modulab | 3 | 0 % |
dtmb | 3 | 0 % |
errosion | 3 | 0 % |
small | 3 | 0 % |
panel | 3 | 0 % |
quality | 3 | 0 % |
delannoy | 3 | 0 % |
cascade | 3 | 0 % |
[pdf] | 3 | 0 % |
oti | 3 | 0 % |
buelow | 3 | 0 % |
gruneisen | 3 | 0 % |
turbines | 3 | 0 % |
surge | 3 | 0 % |
developed | 3 | 0 % |
fedsm | 3 | 0 % |
ballast | 3 | 0 % |
a8 | 3 | 0 % |
generalized | 3 | 0 % |
angle | 3 | 0 % |
camera | 3 | 0 % |
vessel | 3 | 0 % |
or | 3 | 0 % |
capture | 3 | 0 % |
fortes | 3 | 0 % |
interaction | 3 | 0 % |
inside | 3 | 0 % |
reboud | 3 | 0 % |
wavelet | 3 | 0 % |
pictures | 3 | 0 % |
history | 3 | 0 % |
waves | 3 | 0 % |
accelerometer | 3 | 0 % |
steady | 3 | 0 % |
hybrid | 3 | 0 % |
generation | 3 | 0 % |
resistance | 3 | 0 % |
photography | 3 | 0 % |
lagrangian | 3 | 0 % |
coupling | 3 | 0 % |
joint-time | 3 | 0 % |
senocak | 3 | 0 % |
development | 3 | 0 % |
control | 3 | 0 % |
feng | 3 | 0 % |
discharge | 3 | 0 % |
break | 3 | 0 % |
negative | 3 | 0 % |
tanguay | 3 | 0 % |
during | 3 | 0 % |
pustoshny | 3 | 0 % |
mod | 3 | 0 % |
rudders | 3 | 0 % |
chahine | 3 | 0 % |
cloud | 3 | 0 % |
prototype | 3 | 0 % |
chimera | 3 | 0 % |
monatomic | 3 | 0 % |
cavitaion | 3 | 0 % |
fourth | 3 | 0 % |
francis | 3 | 0 % |
cavities | 3 | 0 % |
steel | 3 | 0 % |
generator | 3 | 0 % |
airfoil | 3 | 0 % |
damping | 3 | 0 % |
clearance | 3 | 0 % |
void | 3 | 0 % |
radial | 3 | 0 % |
schnerr | 3 | 0 % |
helium | 3 | 0 % |
bubbly | 3 | 0 % |
govindarajan | 3 | 0 % |
unstructured | 3 | 0 % |
stream | 3 | 0 % |
s | 3 | 0 % |
partial | 3 | 0 % |
i | 3 | 0 % |
nitrogen | 3 | 0 % |
tulin | 3 | 0 % |
around | 3 | 0 % |
sensor | 3 | 0 % |
supercavity | 3 | 0 % |
circular | 3 | 0 % |
grekula | 3 | 0 % |
installation | 3 | 0 % |
66 | 3 | 0 % |
calculate | 3 | 0 % |
leading | 3 | 0 % |
dumont | 3 | 0 % |
abstract | 3 | 0 % |
preconditioning | 3 | 0 % |
diameter | 3 | 0 % |
particles | 3 | 0 % |
leakage | 3 | 0 % |
kueny | 3 | 0 % |
slender | 3 | 0 % |
charles | 2 | 0 % |
projectile | 2 | 0 % |
finite | 2 | 0 % |
expanding | 2 | 0 % |
tomita | 2 | 0 % |
merine | 2 | 0 % |
thermodynamic | 2 | 0 % |
wall | 2 | 0 % |
incipient | 2 | 0 % |
yuriy | 2 | 0 % |
reduce | 2 | 0 % |
froude | 2 | 0 % |
figures | 2 | 0 % |
kubota | 2 | 0 % |
nasa | 2 | 0 % |
recovery | 2 | 0 % |
re | 2 | 0 % |
microbubble | 2 | 0 % |
computational | 2 | 0 % |
attached | 2 | 0 % |
coutier-delgosha | 2 | 0 % |
advances | 2 | 0 % |
caltech | 2 | 0 % |
stainless | 2 | 0 % |
structural | 2 | 0 % |
comparaison | 2 | 0 % |
coalescence | 2 | 0 % |
rake | 2 | 0 % |
focused | 2 | 0 % |
equations | 2 | 0 % |
gate | 2 | 0 % |
flowmeter | 2 | 0 % |
explosion | 2 | 0 % |
presentations | 2 | 0 % |
weber | 2 | 0 % |
change | 2 | 0 % |
henda | 2 | 0 % |
introuduction | 2 | 0 % |
kavitation | 2 | 0 % |
naca0015 | 2 | 0 % |
conditions | 2 | 0 % |
series | 2 | 0 % |
spectra | 2 | 0 % |
occur | 2 | 0 % |
bucket | 2 | 0 % |
thickness | 2 | 0 % |
observation | 2 | 0 % |
implosion | 2 | 0 % |
1 | 2 | 0 % |
stress | 2 | 0 % |
rayleigh-plesset | 2 | 0 % |
reducing | 2 | 0 % |
swept | 2 | 0 % |
parameter | 2 | 0 % |
de | 2 | 0 % |
entrant | 2 | 0 % |
wing | 2 | 0 % |
contact | 2 | 0 % |
oxygen | 2 | 0 % |
sheet/cloud | 2 | 0 % |
radius | 2 | 0 % |
behavior | 2 | 0 % |
breaking | 2 | 0 % |
p | 2 | 0 % |
ices | 2 | 0 % |
photo | 2 | 0 % |
river | 2 | 0 % |
naca66 | 2 | 0 % |
kerwin | 2 | 0 % |
vibrations | 2 | 0 % |
mccormick | 2 | 0 % |
over | 2 | 0 % |
dimensional | 2 | 0 % |
patella | 2 | 0 % |
fluids | 2 | 0 % |
naval | 2 | 0 % |
length | 2 | 0 % |
notes | 2 | 0 % |
intensity | 2 | 0 % |
circle | 2 | 0 % |
displacement | 2 | 0 % |
propellor | 2 | 0 % |
impact | 2 | 0 % |
aisi | 2 | 0 % |
torpedo | 2 | 0 % |
thermometer | 2 | 0 % |
jessup | 2 | 0 % |
through | 2 | 0 % |
finite-volume | 2 | 0 % |
djeridi | 2 | 0 % |
foil | 2 | 0 % |
rise | 2 | 0 % |
table | 2 | 0 % |
maitre | 2 | 0 % |
based | 2 | 0 % |
digital | 2 | 0 % |
atomization | 2 | 0 % |
vanes | 2 | 0 % |
function | 2 | 0 % |
channel | 2 | 0 % |
propulsion | 2 | 0 % |
solution | 2 | 0 % |
radiated | 2 | 0 % |
simplified | 2 | 0 % |
device | 2 | 0 % |
conditions; | 2 | 0 % |
given | 2 | 0 % |
deviation | 2 | 0 % |
v | 2 | 0 % |
jump | 2 | 0 % |
agostino | 2 | 0 % |
shape | 2 | 0 % |
young | 2 | 0 % |
spiral | 2 | 0 % |
simonin | 2 | 0 % |
physical | 2 | 0 % |
kaprantsev | 2 | 0 % |
working | 2 | 0 % |
phenomenon | 2 | 0 % |
determining | 2 | 0 % |
vortexing | 2 | 0 % |
thierry | 2 | 0 % |
conical | 2 | 0 % |
j. | 2 | 0 % |
comparison | 2 | 0 % |
nozzles | 2 | 0 % |
- | 2 | 0 % |
2000 | 2 | 0 % |
fft | 2 | 0 % |
narrow | 2 | 0 % |
spark | 2 | 0 % |
order | 2 | 0 % |
piv | 2 | 0 % |
0015 | 2 | 0 % |
kunz | 2 | 0 % |
shedding | 2 | 0 % |
naca0009 | 2 | 0 % |
barnaby | 2 | 0 % |
cd | 2 | 0 % |
nagahara | 2 | 0 % |
munchen | 2 | 0 % |
pattern | 2 | 0 % |
why | 2 | 0 % |
angles | 2 | 0 % |
d | 2 | 0 % |
geometrical | 2 | 0 % |
engineering | 2 | 0 % |
list | 2 | 0 % |
yu.n | 2 | 0 % |
applications | 2 | 0 % |
laser-induced | 2 | 0 % |
foam | 2 | 0 % |
cryogens | 2 | 0 % |
stage | 2 | 0 % |
kvaerner | 2 | 0 % |
yin | 2 | 0 % |
physics | 2 | 0 % |
fall | 2 | 0 % |
internal | 2 | 0 % |
cryogenic | 2 | 0 % |
turbomachines | 2 | 0 % |
maneuver | 2 | 0 % |
et | 2 | 0 % |
images | 2 | 0 % |
occurred | 2 | 0 % |
o. | 2 | 0 % |
three | 2 | 0 % |
s55c | 2 | 0 % |
band | 2 | 0 % |
simulations | 2 | 0 % |
stuart | 2 | 0 % |
sato | 2 | 0 % |
vapour | 2 | 0 % |
tests | 2 | 0 % |
turbulence | 2 | 0 % |
mie | 2 | 0 % |
burrill | 2 | 0 % |
minilase | 2 | 0 % |
g | 2 | 0 % |
temperature | 2 | 0 % |
open | 2 | 0 % |
celerity | 2 | 0 % |
gas | 2 | 0 % |
area | 2 | 0 % |
nicolas | 2 | 0 % |
thruster | 2 | 0 % |
st. | 2 | 0 % |
g134 | 2 | 0 % |
star | 2 | 0 % |
describe | 2 | 0 % |
inanc | 2 | 0 % |
lauterborn | 2 | 0 % |
latest | 2 | 0 % |
thresholds | 2 | 0 % |
definition | 2 | 0 % |
instabilities | 2 | 0 % |
labview | 2 | 0 % |
non-dimensional | 2 | 0 % |
recent | 2 | 0 % |
régiane | 2 | 0 % |
potential | 2 | 0 % |
effiency | 2 | 0 % |
forward | 2 | 0 % |
waterjet | 2 | 0 % |
double | 2 | 0 % |
loss | 2 | 0 % |
sharp | 2 | 0 % |
kuiper | 2 | 0 % |
plasma | 2 | 0 % |
edu | 2 | 0 % |
stroboscopic | 2 | 0 % |
simple | 2 | 0 % |
coupled | 2 | 0 % |
ptv | 2 | 0 % |
cocchi | 2 | 0 % |
preconditioned | 2 | 0 % |
lifting | 2 | 0 % |
hammer | 2 | 0 % |
pods | 2 | 0 % |
most | 2 | 0 % |
henoch | 2 | 0 % |
h | 2 | 0 % |
anthony | 2 | 0 % |
l. | 2 | 0 % |
thin | 2 | 0 % |
lausanne | 2 | 0 % |
rolla | 2 | 0 % |
sonoluminescence | 2 | 0 % |
closure | 1 | 0 % |
dragram | 1 | 0 % |
constrained | 1 | 0 % |
windsurf | 1 | 0 % |
c.-s. | 1 | 0 % |
irregular | 1 | 0 % |
j.e. | 1 | 0 % |
conclusions | 1 | 0 % |
cylinder | 1 | 0 % |
panasonic | 1 | 0 % |
lubricants | 1 | 0 % |
procedure | 1 | 0 % |
storey | 1 | 0 % |
algebraic | 1 | 0 % |
can | 1 | 0 % |
kaplam | 1 | 0 % |
carolyn | 1 | 0 % |
left | 1 | 0 % |
coefficients | 1 | 0 % |
intraluminal | 1 | 0 % |
subsonic | 1 | 0 % |
k | 1 | 0 % |
circular-cylindrical | 1 | 0 % |
presence | 1 | 0 % |
l. | 1 | 0 % |
si | 1 | 0 % |
upon | 1 | 0 % |
plates | 1 | 0 % |
viscosity | 1 | 0 % |
circulating | 1 | 0 % |
j.s.uhlman | 1 | 0 % |
hydropower | 1 | 0 % |
correlation | 1 | 0 % |
moon | 1 | 0 % |
vertical | 1 | 0 % |
ntnu | 1 | 0 % |
venkateswaran | 1 | 0 % |
surfaces | 1 | 0 % |
through-flow | 1 | 0 % |
estimate | 1 | 0 % |
mechanics | 1 | 0 % |
jis | 1 | 0 % |
sheets | 1 | 0 % |
soviet | 1 | 0 % |
fatigue | 1 | 0 % |
c. | 1 | 0 % |
requirements | 1 | 0 % |
generators | 1 | 0 % |
vidéo | 1 | 0 % |
lax | 1 | 0 % |
8 | 1 | 0 % |
98 | 1 | 0 % |
pelton | 1 | 0 % |
laminar | 1 | 0 % |
loaded | 1 | 0 % |
excitation | 1 | 0 % |
machineries | 1 | 0 % |
joint-time-frequency | 1 | 0 % |
latorre | 1 | 0 % |
in. | 1 | 0 % |
numachi | 1 | 0 % |
quasisteady | 1 | 0 % |
vapor | 1 | 0 % |
xavier | 1 | 0 % |
quart | 1 | 0 % |
partially | 1 | 0 % |
quasi-second | 1 | 0 % |
convergence | 1 | 0 % |
gamma | 1 | 0 % |
blads | 1 | 0 % |
spillways | 1 | 0 % |
source | 1 | 0 % |
empirical | 1 | 0 % |
into | 1 | 0 % |
local | 1 | 0 % |
ambient | 1 | 0 % |
c15c | 1 | 0 % |
multi-dimensional | 1 | 0 % |
judge | 1 | 0 % |
0020 | 1 | 0 % |
3% | 1 | 0 % |
rupture | 1 | 0 % |
china | 1 | 0 % |
storage | 1 | 0 % |
helix | 1 | 0 % |
segment | 1 | 0 % |
roll | 1 | 0 % |
0012 | 1 | 0 % |
axis | 1 | 0 % |
ali | 1 | 0 % |
szeri | 1 | 0 % |
procédure | 1 | 0 % |
algorithm | 1 | 0 % |
propulsors | 1 | 0 % |
skew | 1 | 0 % |
extapro | 1 | 0 % |
de-aeration | 1 | 0 % |
allmaras | 1 | 0 % |
liquids | 1 | 0 % |
burril | 1 | 0 % |
pipe? | 1 | 0 % |
adaption | 1 | 0 % |
steek | 1 | 0 % |
staged | 1 | 0 % |
1973 | 1 | 0 % |
multiperforated | 1 | 0 % |
-pumps | 1 | 0 % |
fresh | 1 | 0 % |
c1100 | 1 | 0 % |
isenthalpic | 1 | 0 % |
georges | 1 | 0 % |
loads | 1 | 0 % |
dimensions | 1 | 0 % |
backwards | 1 | 0 % |
elation | 1 | 0 % |
bar | 1 | 0 % |
n] | 1 | 0 % |
depending | 1 | 0 % |
b.f. | 1 | 0 % |
injectors | 1 | 0 % |
reflector | 1 | 0 % |
percentage | 1 | 0 % |
roll-up | 1 | 0 % |
1977 | 1 | 0 % |
pcpan | 1 | 0 % |
nuçeli | 1 | 0 % |
pcjet | 1 | 0 % |
valves. | 1 | 0 % |
resulting | 1 | 0 % |
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uhlman | 1 | 0 % |
valves | 1 | 0 % |
combine | 1 | 0 % |
value | 1 | 0 % |
chalmers | 1 | 0 % |
hitch-hikers | 1 | 0 % |
unstable | 1 | 0 % |
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interact | 1 | 0 % |
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agard-r-827 | 1 | 0 % |
impulsive | 1 | 0 % |
estimating | 1 | 0 % |
propellers” | 1 | 0 % |
kilogram | 1 | 0 % |
jakobsen | 1 | 0 % |
property | 1 | 0 % |
tow | 1 | 0 % |
mikael | 1 | 0 % |
similarity | 1 | 0 % |
inducers | 1 | 0 % |
allintitle | 1 | 0 % |
secondary | 1 | 0 % |
lapse | 1 | 0 % |
some | 1 | 0 % |
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streamline | 1 | 0 % |
born | 1 | 0 % |
serebrvv@public.icyb.kiev.ua | 1 | 0 % |
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dissolved | 1 | 0 % |
akhatov | 1 | 0 % |
constant | 1 | 0 % |
cetrifugal | 1 | 0 % |
wire | 1 | 0 % |
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billard | 1 | 0 % |
berchiche | 1 | 0 % |
aeronaut | 1 | 0 % |
inanç | 1 | 0 % |
interval | 1 | 0 % |
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lectures | 1 | 0 % |
computed | 1 | 0 % |
passive | 1 | 0 % |
ellipsoidal | 1 | 0 % |
mechnism | 1 | 0 % |
entertainment | 1 | 0 % |
research | 1 | 0 % |
center | 1 | 0 % |
slot | 1 | 0 % |
improve | 1 | 0 % |
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space | 1 | 0 % |
perfect | 1 | 0 % |
book | 1 | 0 % |
procedures | 1 | 0 % |
parallel | 1 | 0 % |
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lavrentyev | 1 | 0 % |
simoneau | 1 | 0 % |
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sessiona4.002 | 1 | 0 % |
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“similarities | 1 | 0 % |
incident | 1 | 0 % |
sigma | 1 | 0 % |
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anaylsis | 1 | 0 % |
operating | 1 | 0 % |
co. | 1 | 0 % |
freguency | 1 | 0 % |
dose | 1 | 0 % |
material-removal | 1 | 0 % |
2006 | 1 | 0 % |
stability | 1 | 0 % |
bend | 1 | 0 % |
units | 1 | 0 % |
orlando | 1 | 0 % |
fuel | 1 | 0 % |
azipods | 1 | 0 % |
mixture | 1 | 0 % |
kalumuck | 1 | 0 % |
systems | 1 | 0 % |
runge-kutta | 1 | 0 % |
scattering | 1 | 0 % |
pulsations | 1 | 0 % |
diff | 1 | 0 % |
des | 1 | 0 % |
circulation | 1 | 0 % |
removes | 1 | 0 % |
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6.0 | 1 | 0 % |
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1996 | 1 | 0 % |
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Other words | 539 | 8.3 % |
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