Physics of Fluids,
Journal Year:
2024,
Volume and Issue:
36(7)
Published: July 1, 2024
The
Bradshaw
assumption,
that
the
ratio
of
Reynolds
shear
stress
to
turbulence
kinetic
energy
(TKE)
is
a
constant
roughly
equal
0.3,
introduced
into
eddy
viscosity
and
TKE
dissipation
term
transport
model
(SST).
This
calibrated
by
zero-pressure-gradient
plate
boundary
layer
test.
not
applicable
rotating
separation
flows
in
hydraulic
machinery,
while
its
dynamic
effects
are
usually
ignored.
In
this
article,
comprehensive
evaluation
coefficient
(DBC)
SST
conducted.
First,
theoretical
analyses
existing
typical
DBCs
carried
out,
suitable
expression
form
driven
single
number
adopted
view
well-reflected
high
robustness.
According
equation
structures
SST,
three
strategies
proposed,
including
only
introducing
DBC
(SST-M1),
(SST-M2),
both
(SST-M1
+
M2).
Second,
classical
case
around
hydrofoil
employed
evaluate
application
these
strategies.
results
show
SST-M1
exhibits
severe
lift/drag
oscillations
at
large
angles
attack
accompanied
fluctuations,
indicating
poor
numerical
stability
potential
risk
strategy.
contrast,
SST-M2
M2
can
effectively
improve
deficiencies
overestimating
lift
underestimating
drag
attack,
which
attributed
promotion
earlier
larger
flow
separation.
consistency
between
two
implies
plays
key
role
enhancing
prediction
SST.
Therefore,
strategy
recommended
extend
applicability
for
machinery.
Physics of Fluids,
Journal Year:
2024,
Volume and Issue:
36(1)
Published: Jan. 1, 2024
Tip
leakage
flow
is
one
of
the
significant
factors
influencing
internal
stability
mixed-flow
pumps,
and
in
severe
cases,
it
can
lead
to
channel
blockage
energy
loss.
In
order
gain
a
deeper
understanding
dissipation
mechanism
induced
by
tip
vortex
cavitation,
this
study
based
on
Wray–Agarwal
(WA)
turbulence
model
homogeneous
model,
investigating
cavitation
characteristics
pumps.
Additionally,
entropy
production
theory
employed
evaluate
losses
within
pump
analyze
components
loss
impeller
guide
vanes.
The
research
results
reveal
that
with
increasing
intensity,
low-pressure
region
at
leading
edge
blade
extends
toward
trailing
edge,
static
pressure
distribution
blade's
side.
Leakage
spatial
vortices
move
closer
suction
side
intensity.
Cavitation
primarily
affects
region,
turbulent
being
main
source
High
zones
are
concentrated
blade,
correlating
recirculation
trailing-edge
vortices.
This
provides
theoretical
insights
practical
implications
for
enhancing
performance
offering
valuable
guidance
design
operation.
Physics of Fluids,
Journal Year:
2023,
Volume and Issue:
35(12)
Published: Dec. 1, 2023
In
this
study,
we
numerically
examine
the
behavior
of
NACA
(National
Advisory
Committee
for
Aeronautics)
66
hydrofoil
under
combined
oscillatory
motion,
considering
different
cavitation
numbers.
The
large
eddy
simulation
method
is
used
turbulence
modeling.
vertical
oscillation
(combined
oscillation)
creates
an
effective
angle
attack,
leading
to
reduced
drag
force.
Our
findings
indicate
that
increasing
speed
leads
a
delayed
onset
and
increased
production
cavity
clouds.
Moreover,
increase
in
attack
during
motion
decreases
detachment
length
bubbles.
Further
investigations
show
on
hydrofoil's
surface
can
accelerate
shift
from
laminar
turbulent
boundary
layer,
reinforcing
layer's
strength
thereby
delaying
flow
separation.
Additionally,
accurately
terms
vorticity
transport
equation
research.
It
evident
dilatation
term
forms
near
layers
close
correlates
well
with
vapor
volume
fraction.
This
plays
vital
role
inception
process.
Journal of Fluids Engineering,
Journal Year:
2024,
Volume and Issue:
146(6)
Published: Feb. 22, 2024
Abstract
To
simulate
the
microscale
bubble
distribution
and
its
effect
on
high-frequency
cavitation
noise,
we
present
a
two-way
transition
coupling
Euler–Lagrange
model.
The
model
accounts
for
both
cavity
fission
environmental
nucleation
as
sources
of
bubbles,
which
are
limited
in
traditional
mesh-based
Euler
models.
We
evaluate
with
experimental
data
truncated
NACA0009
hydrofoil
well
measured
size
distributions,
showing
satisfactory
results
velocity
distribution,
patterns,
power
law
scalings
size.
Based
an
acoustic
analogy,
find
that
produces
sound
waves
smaller
wavelengths
higher
frequencies
than
model,
mainly
attributed
to
two
factors:
(1)
bubbles
high
natural
frequency
(2)
intense
multiple
collapse/rebound
behavior.
This
is
promising
predicting
full-spectrum
noise.
Physics of Fluids,
Journal Year:
2023,
Volume and Issue:
35(12)
Published: Dec. 1, 2023
The
underwater
vehicle
is
subjected
to
complex
hydrodynamic
loads
during
water-exit
process,
which
seriously
affect
the
structural
strength
and
stability
of
vehicle.
This
paper
investigates
effect
high-pressure
venting
conditions
on
dynamic
evolution
characteristics
cavity
completely
free
a
based
self-designed
experiments.
Some
novel
phenomena
are
found
in
experiment,
hypothesis
constant
acceleration
established
explain
formation
mechanism.
results
reveal
that
reentrant
jet
main
factor
influencing
pattern
development
causes
great
differences
between
partial
supercavity
states.
balance
initial
volume
increase
gas
leakage
rate
fact
increasing
launch
Froude
number
state
does
not
cause
significant
changes
size.
There
stable
interval
0.0038
0.03
for
entrainment
coefficient
cavity.
influence
morphology
varies
within
different
ranges.
Besides,
six
patterns
closure
conditions.
coupling
interaction
vortex
tube
most
process.
intervals
roughly
same.
present
study
aims
provide
reference
active
flow
control
water-exit.
Physics of Fluids,
Journal Year:
2024,
Volume and Issue:
36(5)
Published: May 1, 2024
In
this
work,
a
National
Advisory
Committee
for
Aeronautics
66
hydrofoil
with
leading-edge
protuberances
is
designed.
The
large
eddy
simulation
combined
the
Schnerr–Sauer
cavitation
model
used
to
obtain
satisfactory
result
as
compared
experimental
measurement,
integrating
permeable
Ffowcs
Williams–Hawkings
equation
cavitation-induced
noise
analysis.
It
found
that
special
geometric
structure
deflects
incoming
flow,
creating
two
counter-rotating
streamwise
vortices
at
peak
shoulders.
These
lead
upwash
and
downwash
effects
alter
pressure
distribution
on
suction
side.
low
localized
in
trough
facilitates
advancement
of
while
severely
limiting
spanwise
development
cloud
cavity,
shortening
evolution
by
about
20%
reducing
maximum
volume
35%.
Analysis
using
vorticity
transport
indicates
different
splitting
terms
play
dominant
roles
stages
evolution.
Although
induces
disturbances
primary
vortex,
effect
limited.
Acoustic
shows
bionic
can
reduce
total
sound
level
7.8–8.3
dB.
spherical
reduction
not
effective
expected
due
similar
acceleration
processes
hydrofoils.
However,
fluctuation
caused
collapse
cavity
reduced
suppression,
which
reduces
linear
noise.
addition,
suppress
generation
large-scale
vortex
systems
transform
them
into
smaller
ones,
resulting
correlation
coherence
shedding
vortices.
This
critical
factor
reduction.
Finally,
we
hypothesize
unstable
related
regions.
increase
momentum
exchange
within
boundary
layer,
affecting
its
stability
weakening
acoustic
feedback
loop.